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United States National Advisory Committee for Aeronautics

(United States. National Advisory Committee for Aeronautics)

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• United States. National Advisory Committee for Aeronautics: Annual Report of the National Advisory Committee for Aeronautics (partial serial archives)

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Additional books from the extended shelves:

• United States. National Advisory Committee for Aeronautics: [Reports and memoranda presented to the National Advisory Committee for Aeronautics, 1914-192?] (1914) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Accelerations in fighter-airplane crashes (National Advisory Committee for Aeronautics, 1957), also by Loren W. Acker, Jacob C. Moser, and Dugald O. Black (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Accuracy of airspeed measurements and flight calibration procedures (National Advisory Committee for Aeronautics, 1948), also by Wilber B. Huston (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Achromatization of Debye-Scherrer lines (National Advisory Committee for Aeronautics, 1951), also by Hans Ekstein and Stanley Siegel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Acoustics of a nonhomogeneous moving medium (National Advisory Committee for Aeronautics, 1956), also by D. I. Blokhint�sev (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Additional measurements of the drag of surface irregularities in turbulent boundary layers (NACA, 1951), also by W. Tillmann (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Aeration of aircraft lubricating oils over a range of temperature (National Advisory Committee for Aeronautics, 1949), also by W. W. Woods and J. V. Robinson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Alan B. Kehlet and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4 (National Advisory Committee for Aeronautics, 1956), also by Earl D. Knechtel, Arvid N. Andrea, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by William C. Sleeman, Robert E. Becht, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88 (National Advisory Committee for Aeronautics, 1951), also by John A. Kelly, Nora-Lee F. Hayter, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics of a spoiler-slot-deflector control on a 45° sweptback wing at Mach numbers of 1.61 and 2.01 (National Advisory Committee for Aeronautics, 1957), also by Douglas R. Lord, Robert Moring, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by Boyd C. Myers, Thomas J. King, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds (National Advisory Committee for Aeronautics, 1949), also by Bernard N. Daley, Douglas R. Lord, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic characteristics of three planing-tail flying-boat hulls (National Advisory Committee for Aeronautics, 1947), also by Campbell C. Yates and John M. Riebs (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Aerodynamic characteristics of three tapered airfoils tested in the Variable Density Wind Tunnel (National Advisory Committee for Aeronautics ;, 1931), also by Raymond F. Anderson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The aerodynamic effects of wing cut-outs (Government Printing Office, 1934), also by Albert Sherman (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Aerodynamic heating and the deflection of drops by an obstacle in an air stream in relation to aircraft icing (National Advisory Committee for Aeronautics ;, 1940), also by Arthur Kantrowitz (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 (National Advisory Committee for Aeronautics, 1955), also by Charles B. Rumsey, Russell N. Hopko, Robert O. Piland, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components (National Advisory Committee for Aeronautics, 1950), also by Macon C. Ellis, Carl E. Grigsby, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45° sweptback wing at transonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Donald D. Arabian, Charles F. Reid, Jack F. Runckel, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Air admixture to exhaust jets (NACA, 1953), also by Eugen Sänger (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Air-water analogy and the study of hydraulic models (National Advisory Committee for Aeronautics, 1953), also by Giulio Supino (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aircraft accidents : methods of analysis (Government Printing Office, 1929), also by Subdivison Special Committee on the Nomenclature (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aircraft circular (National Advisory Committee for Aeronautics, 1926) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aircraft Circulars (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Aircraft configurations developing high lift-drag ratios at high supersonic speeds (NACA, 1956), also by A. J. Eggers, Clarence A. Syvertson, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Airfoil theory at supersonic speed (National Advisory Committee for Aeronautics, 1939), also by H. Schlichting (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Airplane measurements of atmospheric turbulence for altitudes between 20,000 and 55,000 feet over the Western part of the United States (National Advisory Committee for Aeronautics, 1957), also by Thomas L. Coleman and Emilie C. Coe (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by Gareth H. Jordan, Stanley P. Butchart, Earl R. Keener, Flight Research Center (U.S.), and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Amplitudenverteilung und energiebilanz der kleinen störungen bei der plattenströmung (National Advisory Committee for Aeronautics, 1950), also by H. Schlichting (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analog study of a shock-position diffuser control on a supersonic turbojet engine (National Advisory Committee for Aeronautics, 1956), also by David Novik, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analog study of interacting and noninteracting multiple-loop control systems for turbojet engines (National Advisory Committee for Aeronautics, 1954), also by George J. Pack and W. E. Phillips (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of altitude compensation systems for aircraft carburetors (National Advisory Committee for Aeronautics, 1949), also by Edward W. Otto (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of an axial compressor stage with infinitesimal and finite blade spacing (National Advisory Committee for Aeronautics, 1951), also by H. J. Reissner and L. Meyerhoff (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), also by Reece V. Hensley and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of compressor performance (National Advisory Committee for Aeronautics, 1948), also by Robert O. Dietz, John K. Kuenzig, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analysis of control requirements and control parameters for direct-coupled turbojet engines (National Advisory Committee for Aeronautics, 1948), also by David Novik, Edward W. Otto, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of ejector thrust by integration of calculated surface pressures (National Advisory Committee for Aeronautics, 1949), also by John C. Sanders and Virginia L. Brightwell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes (NACA, 1944), also by Marvin Pitkin and Bernard Maggin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8 (National Advisory Committee for Aeronautics, 1954), also by Richard H. Cavicchi, Robert E. English, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of plane-stress problems with axial symmetry in strain-hardening range (National Advisory Committee for Aeronautics, 1950), also by M. H. Lee Wu (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of propeller efficiency losses associated with heated-air thermal de-icing (National Advisory Committee for Aeronautics ;, 1946), also by Blake W. Corson and Julian D. Maynard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of properties of foam (National Advisory Committee for Aeronautics, 1949), also by J. W. McBain, A. P. Brady, and Sydney Ross (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of temperature distribution in liquid-cooled turbine blades (National Advisory Committee for Aeronautics, 1951), also by John N. B. Livingood and W. Byron Brown (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analysis of the applicability of the hypersonic similarity law to the study of flow about bodies of revolution at zero angle of attack (National Advisory Committee for Aeronautics, 1950), also by Dorris M. Ehret, Victor I. Stevens, and Vernon J. Rossow (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analysis of the autorotative performance of a helicopter powered by rotor-tip jet units (National Advisory Committee for Aeronautics, 1950), also by Alfred Gessow (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane (National Advisory Committee for Aeronautics, 1951), also by Richard B. Skoog and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of the effects of boundary-layer control on the power-off landing performance characteristics of a liaison type of airplane (National Advisory Committee for Aeronautics, 1950), also by Elmer A. Horton, Stanley F. Racisz, and Laurence K. Loftin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of the effects of boundary-layer control on the take-off performance characteristics of a liaison-type airplane (National Advisory Committee for Aeronautics, 1948), also by Elmer A. Horton and John H. Quinn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of the effects of design pressure ratio per stage and off-design efficiency on the operating range of multistage axial-flow compressors (National Advisory Committee for Aeronautics, 1950), also by Melvyn Savage and Willard R. Westphal (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability below the Mach Number of Lift Divergence (National Advisory Committee for Aeronautics, 1948), also by John A. Axelson and J. Conrad Crown (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of the effects of wing interference on the tail contributions to the rolling derivatives (National Advisory Committee for Aeronautics, 1951), also by William H. Michael (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analysis of the relation between horizontal temperature variations and maximum effective gust velocities in thunderstorms (National Advisory Committee for Aeronautics, 1949), also by H. Press and J. K. Thompson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of turbine performance and effect of tail-pipe design on engine performance (National Advisory Committee for Aeronautics, 1948), also by Richard P. Krebs, Frederick C. Foshag, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of turbine performance of 19B-8 engine (National Advisory Committee for Aeronautics, 1948), also by Richard P. Krebs, Frank L. Suozzi, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of turbulent free-convection boundary layer on flat plate (National Advisory Committee for Aeronautics, 1950), also by E. R. G. Eckert and Thomas W. Jackson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages (National Advisory Committee for Aeronautics, 1953), also by Robert G. Diessler and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers (National Advisory Committee for Aeronautics, 1954), also by Robert G. Deissler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical and experimental investigation of a forced-convection air-cooled internal strut-supported turbine blade (National Advisory Committee for Aeronautics, 1954), also by Eugene F. Schum and Francis S. Stepka (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical and experimental investigation of effect of twist on vibrations of cantilever beams (National Advisory Committee for Aeronautics, 1951), also by Alexander Mendelson and Selwyn Gendler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions (National Advisory Committee for Aeronautics, 1950), also by Alexander Mendelson and Selwyn Gendler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades (National Advisory Committee for Aeronautics, 1951), also by William R. Slivka, David H. Silvern, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical investigation of fuel temperatures and fuel-evaporation losses encountered in long-range high-altitude supersonic flight (National Advisory Committee for Aeronautics, 1953), also by Richard J. McCafferty and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical investigation of some three-dimensional flow problems in turbomachines (National Advisory Committee for Aeronautics, 1952), also by Frank E. Marble and Irving Michelson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical investigation of turbulent flow in smooth tubes with heat transfer with variable fluid properties for Prandtl number of 1 (National Advisory Committee for Aeronautics, 1950), also by Robert G. Deissler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical investigation of two liquid cooling systems for turbine blades (National Advisory Committee for Aeronautics, 1951), also by Thomas W. Jackson, John N. B. Livingood, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical method for determining transmission and absorption of time-dependent radiation through thick absorbers. [Part] 1, Radioactivity of absorber, time-dependent (National Advisory Committee for Aeronautics, 1949), also by G. Allen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical method for determining transmission and absorption of time-dependent radiation through thick absorbers. [Part] 2, Source intensity, time-dependent (National Advisory Committee for Aeronautics, 1949), also by G. Allen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analytical study of heat requirements for icing protection of radomes (National Advisory Committee for Aeronautics, 1953), also by James P. Lewis and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical study of shimmy of airplane wheels (NACA, 1952), also by Christian Bourcier de Carbon (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An analytical study of the effect of airplane wake on the lateral dispersion of aerial sprays (National Advisory Committee for Aeronautics, 1953), also by Wilmer H. Reed (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Analytical study of the equilibrium thickness of boric oxide deposits on jet-engine surfaces (National Advisory Committee for Aeronautics, 1957), also by Paul C. Setze, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Annual report ... including technical reports. (U. S. Govt. Print. Off., 1915) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Annual report including Technical reports. (U.S. Govt. Print. Off., 1915) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Annual report - National Advisory Committee for Aeronautics. (U.S. Govt. Print. Off., 1915) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Apparatus for measurements of time and space correlation (NACA, 1955), also by Alexandre Favre, R. Dumas, and J. Gaviglio (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90° of turning (National Advisory Committee for Aeronautics, 1952), also by John D. Stanitz and Leonard J. Sheldrake (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Application of fuel-air-ratio and initial-temperature data to ignition theory. (National Advisory Committee for Aeronautics, 1955), also by Clyde C. Swett (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems (National Advisory Committee for Aeronautics, 1955), also by Howard J. Curfman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: The Application of the statistical theory of extreme values to gust-load problems (National Advisory Committee for Aeronautics, 1949), also by Harry Press (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Applications of Von Karman's integral method in supersonic wing theory (National Advisory Committee for Aeronautics, 1951), also by Chieh-Chien Chang (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Appraisal of method of flutter analysis based on chosen modes by comparison with experiment for cases of large mass coupling (National Advisory Committee for Aeronautics, 1949), also by Donald S. Woolston and Harry L. Runyan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Approximate corrections for the effects of compressibility on the subsonic stability derivatives of swept wings (National Advisory Committee for Aeronautics, 1949), also by Lewis R. Fisher (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An approximate method for calculation of the laminar boundary layer with suction for bodies of arbitrary shape (NACA, 1949), also by H. Schlichting (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow (NACA, 1949), also by Coleman duP. Donaldson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Approximate method of integration of laminar boundary layer in incompressible fluid (NACA, 1951), also by L. G. Loĭt�si�anskiĭ (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds (National Advisory Committee for Aeronautics, 1958), also by Raymond C. Savin and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Approximate turbulent boundary-layer development in plane compressible flow along thermally insulated surfaces with application to supersonic-tunnel contour correction (National Advisory Committee for Aeronautics, 1950), also by Maurice Tucker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Attainable circulation of airfoils in cascade (National Advisory Committee for Aeronautics, 1949), also by Arthur W. Goldstein and Artur Mager (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Attempts to defoam existing oils by processing (National Advisory Committee for Aeronautics, 1949), also by J. W. McBain, I. M. Abrams, W. W. Woods, and J. V. Robinson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Author index to Index of NACA technical publications, 1915-1949 (NACA, 1970), also by United States. National Advisory Committee for Aeronautics. Division of Research Information, Ruth L. Jackson, and Eugene Bernard Jackson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Autogenous welding in airplane construction (NACA, 1929), also by Ludwig Kuchel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Average bond energies between boron and elements of the fourth, fifth, sixth, and seventh groups of the periodic table (National Advisory Committee for Aeronautics, 1955), also by A. P. Altshuller, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10) (National Advisory Committee for Aeronautics, 1953), also by Elmo J. Mottard and J. Dan Loposer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Axial-load fatigue properties of 24S-T and 75S-T aluminum alloy as determined in several laboratories (National Advisory Committee for Aeronautics, 1953), also by Charles B. Landers, Paul Kuhn, W. S. Hyler, and H. J. Grover (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Axisymmetric supersonic flow in rotating impellers (National Advisory Committee for Aeronautics, 1951), also by Arthur W. Goldstein (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A balanced-pressure sliding seal for transfer of pressurized air between stationary and rotating parts (National Advisory Committee for Aeronautics, 1957), also by Arthur N. Curren and Reeves P. Cochran (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Bearing strengths of some aluminum-alloy permanent-mold castings (National Advisory Committee for Aeronautics, 1951), also by E. M. Finley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Behavior of a cantilever plate under rapid-heating conditions (National Advisory Committee for Aeronautics, 1955), also by Louis F. Vosteen and Kenneth James Fuller (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: The Behavior of conventional airplanes in situations thought to lead to most crashes (National Advisory Committee for Aeronautics ;, 1931), also by Fred E. Weick (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Behavior of the laminar boundary layer for periodically oscillating pressure variation (NACA, 1949), also by August Wilhelm Quick and K. Schröder (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Bending stresses due to torsion in cantilever box beams (National Advisory Committee for Aeronautics, 1935), also by Paul Kuhn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Bibliography of aeronautics. (Gov't Printing Off., 1909), also by Paul Brockett (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Bibliography of aeronautics. (Government Printing Office, 1916), also by Paul Brockett (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Bibliography of aeronautics. (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Bibliography of unclassified aircraft-fire literature (National Advisory Committee for Aeronautics, 1949), also by Solomon Weiss and Lewis Flight Propulsion Laboratory (U.S.) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Blade-to-coolant heat-transfer results and operating data from a natural-convection water-cooled single-stage turbine (National Advisory Committee for Aeronautics, 1951), also by Anthony J. Diaguila, John C. Freche, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Boundary layer (National Advisory Committee for Aeronautics, 1956), also by L. G. Loĭt�si�anskiĭ (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Boundary-layer measurements on several porous materials with suction applied (National Advisory Committee for Aeronautics, 1952), also by George B. McCullough, Bruno J. Gambucci, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Buckling of thin-walled cylinder under axial compression and internal pressure (National Advisory Committee for Aeronautics, 1950), also by Hsu Lo, Edward B. Schwartz, and Harold Crate (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring (National Advisory Committee for Aeronautics, 1957), also by Fred B. Sutton, J. Walter Lautenberger, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane (National Advisory Committee for Aeronautics, 1955), also by John P. Campbell, Carroll H. Woodling, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Calculation of compressible potential flow past slender bodies of revolution by an integral method (National Advisory Committee for Aeronautics, 1950), also by Milton M. Klein and W. Perl (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Calculation of downwash behind supersonic wings with an application to triangular plan forms (National Advisory Committee for Aeronautics, 1948), also by Max A. Heaslet and Harvard Lomax (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculation of load distribution in stiffened cylindrical shells (National Advisory Commitee for Aeronautics, 1938), also by Hans Ebner and H. Koller (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The calculation of span load distributions on swept-back wings (National Advisory Committee for Aeronautics ;, 1941), also by William Mutterperl (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculation of surface temperatures in steady supersonic flight (National Advisory Committee for Aeronautics ;, 1946), also by George P. Wood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness (National Advisory Committee for Aeronautics, 1949), also by Franklin W. Diederich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculation of the shape of a two-dimensional supersonic nozzle in closed form (NACA, 1953), also by Dante Cunsolo (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculation of turbulent expansion processes (NACA, 1945), also by Walter Tollmien (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calculations of the performance of a compression-ignition engine-compressor turbine combination. [Part] 2, Performance of complete combination (National Advisory Committee for Aeronautics, 1947), also by Alexander Mendelson and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Calibration of strain-gage installations in aircraft structures for the measurement of flight loads (National Advisory Committee for Aeronautics, 1953), also by T. H. Skopinski, Wilber B. Huston, and William S. Aiken (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Carbon-deposition characteristics of MIL-F-5624A fuels containing high-boiling aromatic hydrocarbons (National Advisory Committee for Aeronautics, 1952), also by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Carbon deposition obtained with MIL-F-5624A fuels in a single combustor and in three full-scale engines (National Advisory Committee for Aeronautics, 1954), also by Jerrold D. Wear and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Carbon deposition of several special turbojet-engine fuels (National Advisory Committee for Aeronautics, 1951), also by Jerrold D. Wear, James W. Useller, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Carburetor design : a preliminary study of the state of the art (U.S. Govt. Print. Off., 1917), also by Charles Edward Lucke (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Characteristics of a single float seaplane during take-off (Government Printing Office, 1925), also by J. W. Crowley and K. M. Ronan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Characteristics of Clark Y airfoils of small aspect ratios (Government Printing Office, 1932), also by C. H. Zimmerman (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration (National Advisory Committee for Aeronautics, 1955), also by A. James Vitale (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Characteristics of six research wind tunnels of the Ames Aeronautical Laboratory. (Washington, 1957) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance (National Advisory Committee for Aeronautics, 1957), also by John F. Royall and Benjamine J. Garland (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Characteristics of turbulence in a boundary layer with zero pressure gradient (National Advisory Committee for Aeronautics, 1954), also by P. S. Klebanoff (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Charts and approximate formulas for the estimation of aeroelastic effects on the lateral control of swept and unswept wings (National Advisory Committee for Aeronautics, 1952), also by Kenneth A. Foss and Franklin W. Diederich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings (National Advisory Committee for Aeronautics, 1952), also by Franklin W. Diederich and Kenneth A. Foss (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight (National Advisory Committee for Aeronautics, 1954), also by Kenneth B. Amer and Alfred Gessow (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Charts of pressure rise obtainable with airfoil-type axial-flow cooling fans (National Advisory Committee for Aeronautics ;, 1947), also by A. Kahane (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Chordwise and compressibility corrections to slender-wing theory (National Advisory Committee for Aeronautics, 1951), also by Harvard Lomax and Loma Sluder (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A class of de Laval nozzles (National Advisory Committee for Aeronautics, 1949), also by S. V. Falkovich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Collection and analysis of hinge-moment data on control-surface tabs (National Advisory Committee for Aeronautics ;, 1947), also by Paul E. Purser and Charles B. Cook (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Column strength of tubes elastically restrained against rotation at the ends ([Washington] : [U.S. G.P.O], [1938], 1938), also by William R. Osgood (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), also by Bemrose Boyd and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Combustion-chamber performance with four fuels in bumblebee 18-inch ram jet incorporating various rake- or gutter-type flame holders (National Advisory Committee for Aeronautics, 1948), also by Ephraim M. Howard, David T. Dupree, Fred A. Wilcox, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Combustion efficiency and altitude operational limits of three liquid hydrocarbon fuels having high volumetric energy content in a J33 single combustion (National Advisory Committee for Aeronautics, 1950), also by Edward G. Stricker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Combustion of aluminum borohydride in a supersonic wind tunnel (National Advisory Committee for Aeronautics, 1955), also by Edward A. Fletcher, Melvin Gerstein, Robert G. Dorsch, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Combustion of smoke in diffusion and bunsen flames (National Advisory Committee for Aeronautics, 1951), also by Thomas P. Clark and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine (National Advisory Committee for Aeronautics, 1958), also by Marcus F. Heidmann and Louis Baker (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: A comparative analysis of the performance of long-range hypervelocity vehicles (National Advisory Committee for Aeronautics, 1957), also by Alfred J. Eggers, Stanford E. Neice, and H. Julian Allen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparative effectiveness of a convection-type and a radiation-type cooling cap on a turbosupercharger (National Advisory Committee for Aeronautics ;, 1946), also by Frederick J. Hartwig (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparative strengths of some adhesive-adherend systems (National Advisory Committee for Aeronautics, 1949), also by N. J. DeLollis, J. E. Wier, and Nancy Rucker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A comparison at mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizonatl tail heights behind a wing with 45 degrees of sweepback (National Advisory Committee for Aeronautics, 1955), also by Jack D. Stephenson, Angelo Bandettini, Ralph Selan, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of airspeed calibrations evaluated by the accelerometer and radar methods (National Advisory Committee for Aeronautics, 1952), also by Lindsay J. Lina and James P. Trant (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of effectiveness of convection-, transpiration-, and film-cooling methods with air as coolant (National Advisory Committee for Aeronautics, 1953), also by E. R. G. Eckert and John N. B. Livingood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio (National Advisory Committee for Aeronautics, 1958), also by James E. Hatch, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight (NACA, 1953), also by Norman M. McFadden, Harry A. James, John L. McCloud, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of operating characteristics of four experimental and two conventional 75-millimeter-bore cylindrical-roller bearings at high speeds (National Advisory Committee for Aeronautics, 1953), also by William J. Anderson, Zolton N. Nemeth, and E. Fred Macks (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of relative sensitivities of the knock limits of two fuels to six engine variables (National Advisory Committee for Aeronautics ;, 1946), also by Harvey A. Cook, Ernest I. Prichard, and Louis F. Held (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine (National Advisory Committee for Aeronautics, 1957), also by Cavour H. Hauser, William J. Nusbaum, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles (National Advisory Committee for Aeronautics, 1953), also by Milton G. Kofskey, Howard Z. Herzig, and Hubert W. Allen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of the experimental and theoretical distributions of lift on a slender inclined body of revolution at M = 2 (NACA, 1953), also by Edward W. Perkins, Donald M. Kuehn, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory (U.S. G.P.O., 1952), also by Clarence W. Matthews (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps (National Advisory Committee for Aeronautics, 1950), also by Powell M. Lovell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of theoretical and experimental response of a single-mode elastic system in hydrodynamic impact (National Advisory Committee for Aeronautics, 1951), also by Robert W. Miller and Kenneth F. Merten (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of vee-type and conventional tail surfaces in combination with fuselage and wing in the variable-density tunnel (National Advisory Committee for Aeronautics ;, 1941), also by Harry Greenberg (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of weights of 17ST and steel tubular structural members used in aircraft construction (National Advisory Committee for Aeronautics ;, 1931), also by E. C. Hartmann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers (Langley Memorial Aeronautical Laboratory, 1944), also by Robert H. Neely, S. R. Alexander, L. E. Fogarty, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Compatibility of metals with liquid fluorine at high pressures and flow velocities (National Advisory Committee for Aeronautics, 1958), also by Harold W. Schmidt (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Completed tabulation in the United States of tests of 24 airfoils at high Mach numbers (derived from interrupted work at Guidonia, Italy in the 1.31- by 1.74-foot high-speed tunnel) (Washington, 1946), also by Antonio Ferri (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The compressible laminar boundary layer with fluid injection (National Advisory Committee for Aeronautics, 1955), also by George M. Low (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Compression shocks in two-dimensional gas flows (NACA, 1949), also by Adolf Busemann and J. Vanier (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Compressive strength of flanges (National Advisory Committee for Aeronautics, 1950), also by Elbridge Z. Stowell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Compressive tests of a monocoque box (National Advisory Committee for Aeronautics, 1939), also by Walter Ramberg, Samuel Levy, and Albert E. McPherson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall (National Advisory Committee for Aeronautics, 1955), also by Morgan P. Hanson, Andre J. Meyer, Donald F. Johnson, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Concerning the flow about ring-shaped cowlings of finite thickness Part I (NACA, 1952), also by Dietrich Küchemann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Concerning the flow about ring-shaped cowlings. Part II, Annular bodies of infinite length with circulation for smooth entrance (NACA, 1951), also by Dietrich Küchemann and Johanna Weber (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Concerning the flow about ring-shaped cowlings. Part IX, The influence of oblique oncoming flow on the incremental velocities and air forces at the front part of circular cowls (National Advisory Committee for Aeronautics, 1952), also by Dietrich Küchemann and Johanna Weber (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Concerning the flow about ring-shaped cowlings. Part VIII, further measurements on annular profiles (NACA, 1952), also by Dietrich Küchemann and Johanna Weber (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Concerning the flow about ring-shaped cowlings. Part XII, two new classes of circular cowls (NACA, 1953), also by Dietrich Küchemann and Johanna Weber (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Concerning the flow about ring-shaped cowlings. Part XIII, the influence of a projecting hub (NACA, 1953), also by Dietrich Küchemann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Conduction and film cooling of leading and trailing edges of rotor blades (National Advisory Committee for Aeronautics, 1951), also by Vernon L. Arne, Jack B. Esgar, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Considerations on a large hydraulic jet catapult (National Advisory Committee for Aeronautics, 1954), also by Upshur T. Joyner and Walter B. Horne (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow (National Advisory Committee for Aeronautics, 1951), also by Harry L. Runyan and Charles E. Watkins (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Contributions to the theory of the spreading of a free jet issuing from a nozzle (NACA, 1951), also by W. Szablewski (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60° delta wing at Mach numbers of 1.41, 1.62, and 1.96 (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Odell A. Morris and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Control of foaming by adding known mixtures of pure chemicals (National Advisory Committee for Aeronautics, 1949), also by J. W. McBain, R. B. Dean, A. P. Brady, and Sydney Ross (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth (NACA, 1954), also by William K. Koffel and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Cooling of gas turbines [Part] 2, effectiveness of rim cooling of blades (National Advisory Committee for Aeronautics, 1947), also by L. Wolfenstein, John S. McCarthy, Gene L. Meyer, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Cooling of gas turbines [Part] 3, Analysis of rotor and blade temperatures in liquid-cooled gas turbines (National Advisory Committee for Aeronautics, 1947), also by W. Byron Brown, John N. B. Livingood, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Cooling of gas turbines [Part] 4, Calculated temperature distribution in the trailing part of a turbine blade using direct liquid cooling (National Advisory Committee for Aeronautics, 1947), also by W. Byron Brown, William R. Monroe, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Cooling of gas turbines [Part] 5, Effectiveness of air cooling of hollow blades (National Advisory Committee for Aeronautics, 1947), also by L. Wolfenstein, John S. McCarthy, Robert L. Maxwell, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Cooling of gas turbines [Part] 8, Theoretical temperature distributions through gas turbine with special blades and cooling fins on the rim (National Advisory Committee for Aeronautics, 1948), also by W. Byron Brown, John N. B. Livingood, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Copies of slides to be presented for NACA Conference on Automatic Stability and Control of Aircraft, Ames Aeronautical Laboratory, Moffett Field, Calif., March 29 and 30, 1955. (Washington, 1955) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correction factors for wind tunnels of elliptic section with partly open and partly closed test section (NACA, 1951), also by Friedrich Wilhelm Riegels (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation between strength properties in standard test specimens and molded phenolic parts (National Advisory Committee for Aeronautics ;, 1946), also by P. S. Turner and R. H. Thomason (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of calculation and flight studies of the effect of wing flexibility on structural response due to gusts (National Advisory Committee for Aeronautics, 1953), also by John C. Houbolt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of creep-buckling tests with theory (National Advisory Committee for Aeronautics, 1956), also by Sharad A. Patel (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Correlation of cylinder-head temperatures and coolant heat rejections of a multicylinder, liquid-cooled engine of 1710-cubic-inch displacement (U.S. Government Printing Office, 1950), also by Bruce T. Lundin, Louis J. Chelko, and John H. Povolny (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of flight and analog investigations of roll coupling (National Advisory Committee for Aeronautics, 1956), also by Joseph Weil, Richard E. Day, and Flight Research Center (U.S.) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of heat-transfer and friction data for air flowing in inconel tube with rounded entrance (National Advisory Committee for Aeronautics, 1949), also by Warren H. Lowdermilk and Milton D. Grele (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of physical properties of ceramic materials with resistance to fracture by thermal shock (National Advisory Committee for Aeronautics, 1949), also by W. G. Lidman, A. R. Bobrowsky, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of physical properties of ceramic materials with resistance to fracture by thermal shock (National Advisory Committee for Aeronautics, 1949), also by W. G. Lidman and A. R. Bobrowsky (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of physical properties with molecular structure for dicyclic hydrocarbons. [Part] II, 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series (National Advisory Committee for Aeronautics, 1951), also by Irving A. Goodman and Paul H. Wise (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of pilot opinion of stall warning with flight measurements of various factors which produce the warning (National Advisory Committee for Aeronautics, 1949), also by Seth B. Anderson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of supersonic convective heat-transfer coefficients from measurements of the skin temperature of a parabolic body of revolution (NACA RM-10) (NACA, 1951), also by Leo T. Chauvin, Carlos A. de Moraes, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correlation of turbulent heat transfer in a tube for the dissociating system N204 <==> 2N02. (National Advisory Committee for Aeronautics, 1958), also by Richard S. Brokaw, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds (National Advisory Committee for Aeronautics, 1951), also by Sidney M. Harmon (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Corrugated metal diaphragms for aircraft pressure-measuring instruments (National Advisory Committee for Aeronautics ;, 1939), also by W. A. Wildhack and V. H. Goerke (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Creep in metals (National Advisory Committee for Aeronautics, 1952), also by A. D. Schwope, L. R. Jackson, F. R. Shober, and Battelle Memorial Institute (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Creep of lead at various temperatures (National Advisory Committee for Aeronautics, 1951), also by Peter W. Neurath and J. S. Koehler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Andrew Beke, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Critical stress of ring-stiffened cylinders in torsion (National Advisory Committee for Aeronautics, 1949), also by Manuel Stein, Harold Crate, and J. Lyell Sanders (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations (National Advisory Committee for Aeronautics, 1949), also by Harvard Lomax and Max A. Heaslet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Damping in roll of cruciform and some related delta wings at supersonic speeds (National Advisory Committee for Aeronautics, 1951), also by H. S. Ribner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Data on shape and location of detached shock waves on cones and spheres (National Advisory Committee for Aeronautics, 1949), also by Juergen W. Heberle, Paul B. Gooderum, and George P. Wood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings (National Advisory Committee for Aeronautics, 1952), also by Manuel Stein, John M. Hedgepath, and J. Edward Anderson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Design and experimental performance of standard turbine (National Advisory Committee for Aeronautics, 1957), also by Harold E. Rohlik, Herbert W. Scibbe, William T. Wintucky, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed (National Advisory Committee for Aeronautics, 1958), also by Willard R. Westphal, John W. Maynard, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Design method for two-dimensional channels for compressible flow with application to high-solidity cascades (National Advisory Committee for Aeronautics, 1949), also by Sumner Alpert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Design of two-dimensional channels with prescribed velocity distributions along the channel walls. [Part] 2, Solution by Green's function (National Advisory Committee for Aeronautics, 1952), also by John D. Stanitz (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The design of wind tunnels and wind tunnel propellers (G.P.O., 1919), also by Edward P. Warner, C. M. Herbert, and F. H. Norton (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Detailed computational procedure for design of cascade blades with prescribed velocity distributions in compressible potential flows (National Advisory Committee for Aeronautics, 1951), also by George R. Costello, John T. Sinnette, and Robert L. Cummings (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Determination of aromatics and olefins in wide-boiling petroleum fractions (National Aeronautics and Space Administration, 1950), also by A. E. Spakowski, R. R. Hibbard, A. Evans, United States National Aeronautics and Space Administration, and Lewis Flight Propulsion Laboratory (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Determination of blade-to-coolant heat-transfer coefficients on a forced-convection, water-cooled, single-stage turbine (National Advisory Committee for Aeronautics, 1951), also by John C. Freche, Eugene F. Schum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Determination of gas-to-blade convection heat-transfer coefficients on a forced-convection, water-cooled single-stage aluminum turbine (National Advisory Committee for Aeronautics, 1951), also by John C. Freche, Eugene F. Schum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow (National Advisory Committee for Aeronautics, 1953), also by S. Katzoff, Hugh C. DuBose, and M. Frances Faison (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Determination of surge and stall limits of an axial-flow turbojet engine for control applications (National Advisory Committee for Aeronautics, 1953), also by Ross D. Schmidt, Edward W. McGraw, George Vasu, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Determination of the stress concentration factor of a stepped shaft stressed in torsion by means of precision strain gages (NACA, 1947), also by A. Weigand (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Determination of vortex paths by series expansion technique with application to cruciform wings (U.S. Government Printing Office, 1957), also by Alberta Y. Alksne (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of a high-velocity free-flight launcher - the Ames light - gas gun (National Advisory Committee for Aeronautics, 1955), also by A. C. Charters, Vernon J. Rossow, and B. Pat Denardo (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of a laminar boundary layer behind a suction point (NACA, 1952), also by W. Wuest (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of an impinging-jet fuel-injection valve nozzle (National Advisory Committee for Aeronautics ;, 1931), also by J. A. Spanogle (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The development of electrical strain gages (National Advisory Committee for Aeronautics, 1940), also by A. V. De Forest and H. Leaderman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 (National Advisory Committee for Aeronautics, 1956), also by Thomas G. Piercy, Bruce G. Chiccine, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The development of jet-engine Nacelles for a high-speed bomber design (National Advisory Committee for Aeronautics, 1947), also by Robert E. Dannenberg and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of magnesium-cerium forged alloys for elevated-temperature service (National Advisory Committee for Aeronautics, 1951), also by H. C. Cross, C. M. Schwartz, L. W. Eastwood, R. Kaiser, and K. Grube (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane (National Advisory Committee for Aeronautics, 1947), also by Emmet A. Mossman and Donald E. Gault (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Development of turbulence-measuring equipment (National Advisory Committee for Aeronautics, 1953), also by Leslie S. G. Kovásznay (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Diborane, pentaborane, boron, and boron-octene-1 slurries (National Advisory Committee for Aeronautics, 1951), also by Benson E. Gammon (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades (National Advisory Committee for Aeronautics, 1957), also by John C. Houbolt and George W. Brooks (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Diffusion of chromium in alpha-cobalt-chromium solid solutions (National Advisory Committee for Aeronautics, 1950), also by John W. Weeton (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Diffusion of heat from a line source in isotropic turbulence (National Advisory Committee for Aeronautics, 1952), also by M. S. Uberoi and Stanley Corrsin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Dilution of liquid oxygen when nitrogen is used for pressurization (National Advisory Committee for Aeronautics, 1958), also by Thomas G. Walsh, Paul M. Ordin, and R. R. Hibbard (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Direct method of design and stress analysis of rotating disks with temperature gradient (National Advisory Committee for Aeronautics, 1949), also by S. S. Manson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Directional stability characteristics of two types of tandem helicopter fuselage models (National Advisory Committee for Aeronautics, 1954), also by James L. Williams (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A discussion of methods for reducing aerodynamic heating in supersonic flight (National Advisory Committee for Aeronautics, 1955), also by A. J. Jr Eggers and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Displacement effect of the laminar boundary layer and the pressure drag (NACA, 1951), also by Henry Görtler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Downwash characteristics and vortex-sheet shape behind a 63 degree swept-back wing-fuselage combination at a Reynolds number of 6,100,000 (National Advisory Committee for Aeronautics, 1952), also by William H. Tolhurst and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Drag reduction by suction of the boundary layer separated behind shock wave formation at high mach numbers (NACA, 1947), also by B. Regenscheit (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Drop burning rates of hydrocarbon and nonhydrocarbon fuels (National Advisory Committee for Aeronautics, 1957), also by Arthur L. Smith and Charles C. Graves (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Dynamic investigation (National Advisory Committee for Aeronautics, 1949), also by Andre J. Meyer, Howard F. Calvert, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine (National Advisory Committee for Aeronautics, 1956), also by Fred A. Wilcox, Paul Whalen, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Dynamics of mechanical feedback-type hydraulic servomotors under inertia load (National Advisory Committee for Aeronautics, 1952), also by Harold Gold, Victor L. Ransom, and Edward W. Otto (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Ebene potentialströmungen (National Advisory Committee for Aeronautics, 1949), also by Manfred Schäfer, W. Tollmien, and Technische Hochschule Dresden (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing (National Advisory Committee for Aeronautics, 1958), also by Edward C. Polhamus, Kenneth P. Spreemann, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of a 90° cross wind on the take-off distance of a light airplane equipped with a cross-wind landing gear (National Advisory Committee for Aeronautics, 1949), also by Seth B. Anderson, William H. McAvoy, and Burnett L. Gadeberg (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of a reduction in stator solidity on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, R. Y. Wong, Warner L. Stewart, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Robert F. Thompson, Robert T. Taylor, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat (National Advisory Committee for Aeronautics, 1948), also by Roland E. Olson and Norman S. Land (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Effect of an arbitrary surface-temperature variation along a flat plate on the convective heat transfer in an incompressible turbulent boundary layer (National Advisory Committee for Aeronautics, 1951), also by Morris W. Rubesin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of aspect ratio and sweepback on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with retractable ailerons (National Advisory Committee for Aeronautics, 1951), also by Jack Fischel and John R. Hagerman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of aspect ratio on the low-speed lateral control characteristics of unswept untapered low-aspect-ratio wings (National Advisory Committee for Aeronautics, 1951), also by Rodger L. Naeseth and William M. O'Hare (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons (U.S. Government Printing Office, 1952), also by William M. O'Hare, John R. Hagerman, Rodger L. Naeseth, and Jack Fischel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of aspect ratio on undamped torsional oscillations of a thin rectangular wing in supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Charles E. Watkins (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders (National Advisory Committee for Aeronautics, 1934), also by Oscar W. Schey, Vern G. Rollin, and Langley Aeronautical Library (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), also by Charles F. Zalabak, Arthur N. Curren, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4 (NACA, 1952), also by Simon C. Sommer, James A. Stark, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of bronze and nodular iron cage materials on cage slip and other performance characteristics of 75-millimeter-bore cylindrical-roller bearings at DN values of 2 X 10⁶. (National Advisory Committee for Aeronautics, 1953), also by William J. Anderson, Zolton N. Nemeth, and E. Fred Macks (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of cell shape on compressive strength of hexagonal honeycomb structures (National Advisory Committee for Aeronautics, 1950), also by L. A. Ringelstetter, C. B. Norris, and A. W. Voss (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of centrifugal force on flutter of uniform cantilever beam at subsonic speeds with application to compressor and turbine blades (National Advisory Committee for Aeronautics, 1949), also by Alexander Mendelson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of chord size on weight and cooling characteristics of air-cooled turbine blades (National Advisory Committee for Aeronautics, 1957), also by Jack B. Esgar, Arthur N. Curren, and Eugene F. Schum (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of combustor-inlet conditions on performance of an annular turbojet combustor (National Advisory Committee for Aeronautics, 1947), also by J. Howard Childs, Oakley W. Surine, and RIchard J. McCafferty (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of compressibility at high subsonic velocities on the lifting force acting on an elliptic cylinder (National Advisory Committee for Aeronautics ;, 1946), also by Carl Kaplan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel (NACA, 1958), also by Joseph W. Jewel, Robert D. Harrington, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), also by Arthur N. Curren, Charles F. Zalabak, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of diffusion processes and temperature on smoking tendencies of laminar diffusion flames (National Advisory Committee for Aeronautics, 1953), also by Rose L. Schalla and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of dissociation on thermodynamic properties of pure diatomic gases (National Advisory Committee for Aeronautics, 1955), also by Harold W. Woolley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of exhaust pressure on knock-limited performance of an air-cooled aircraft-engine cylinder (National Advisory Committee for Aeronautics, 1948), also by Albert M. Lord, Edward G. Stricker, and Orville H. Heinicke (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of exhaust pressure on the performance of an 18-cylinder air-cooled radial engine with a valve overlap of 62 degrees (National Advisory Committee for Aeronautics ;, 1947), also by Leroy V. Humble, David S. Boman, and Tibor F. Nagey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of free-stream Mach number on gross-force and pumping characteristics of several ejectors (National Advisory Committee for Aeronautics, 1955), also by Leonard E. Stitt and Alfred S. Valerino (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of fuel additives on carbon deposition in a J33 single combustor [Part] 1, Three metallic-organic additives (National Advisory Committee for Aeronautics, 1952), also by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of fuels and fuel-nozzle characteristics on performance of an annular combustor at simulated altitude conditions (National Advisory Committee for Aeronautics, 1948), also by RIchard J. McCafferty and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of heat and power extraction on turbojet-engine performance. 4 - Analytical determination of effects of hot-gas bleed (National Advisory Committee for Aeronautics, 1951), also by Stanley L. Koutz (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of high air velocities on the distribution and penetration of a fuel spray (National Advisory Committee for Aeronautics ;, 1931), also by A. M. Rothrock (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of high pressure on smoking tendency of diffusion flames (National Advisory Committee for Aeronautics, 1954), also by Glen E. McDonald and Rose L. Schalla (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Effect of high shear rate on erosion of common bearing metals (National Advisory Committee for Aeronautics, 1949), also by Charles D. Strang and Thomas P. Clark (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of high viscosity on the flow around a cylinder and around a sphere (NACA, 1952), also by F. Homann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces (National Advisory Committee for Aeronautics, 1951), also by Jacob H. Lichtenstein (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of horizontal-tail size and tail length on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces (National Advisory Committee for Aeronautics, 1951), also by Jacob H. Lichtenstein (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip (National Advisory Committee for Aeronautics, 1953), also by Donald R. Riley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of length-beam ratio on aerodynamic characteristics of flying-boat hulls without wing interference (National Advisory Committee for Aeronautics, 1948), also by John G. Lowry and John M. Riebe (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45° sweptback wing-fuselage model (National Advisory Committee for Aeronautics, 1953), also by William Solomon and James W. Schmeer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of Mach number on the flow and application of compressibility corrections in a two-dimensional subsonic-transonic compressor cascade having varied porous-wall suction at the blade tips (National Advisory Committee for Aeronautics, 1952), also by William B. Briggs (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of nonuniform temperature distributions on the stresses and distortions of stiffened-shell structures (National Advisory Committee for Aeronautics, 1950), also by Richard R. Heldenfels (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of open circular holes on tensile strength and elongation of sheet specimens of some aluminum alloys (National Advisory Committee for Aeronautics, 1949), also by H. N. Hill and R. S. Barker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of orifice length-diameter ratio on the coefficient of discharge of fuel-injection nozzles (National Advisory Committee for Aeronautics ;, 1931), also by A. G. Gelalles and E. T. Marsh (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of pressure on smoking tendency of diffusion flames (National Advisory Committee for Aeronautics, 1953), also by Rose L. Schalla, Glen E. McDonald, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800 degrees R (National Advisory Committee for Aeronautics, 1948), also by Robert C. Kohl, Robert G. Larkin, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of properties of primary fluid on performance of cylindrical shroud ejectors (National Advisory Committee for Aeronautics, 1954), also by Fred D. Kochendorfer and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of quadratic terms in differential equations of atmospheric oscillatons (National Advisory Committee for Aeronautics, 1951), also by C. L. Pekeris (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of reducing valve overlap on engine and compound-power-plant performance (National Advisory Committee for Aeronautics, 1948), also by David S. Boman and Samuel J. Kaufman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Effect of simulated icing on propeller performance (National Advisory Committee for Aeronautics ;, 1946), also by Blake W. Corson and Julian D. Maynard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Effect of small variations in profile of airfoils (National Advisory Committee for Aeronautics ;, 1931), also by Kenneth E. Ward (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of some present-day airplane design trends on requirements for lateral stability (National Advisory Committee for Aeronautics ;, 1941), also by M. J. Bamber (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of surface-active additives on physical behavior of 50-percent slurries of 1.5-micron magnesium in n-decane (National Advisory Committee for Aeronautics, 1955), also by Murray L. Pinns and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of surface roughness on characteristics of spherical shock waves (National Advisory Committee for Aeronautics, 1955), also by Paul W. Huber, Donald R. McFarland, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings (National Advisory Committee for Aeronautics, 1949), also by Warren A. Tucker and Robert L. Nelson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of transverse shear and rotary inertia on the natural frequency of a uniform beam (National Advisory Committee for Aeronautics, 1949), also by Edwin T. Kruszewski (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of variable viscosity and thermal conductivity on high-speed slip flow between concentric cylinders (National Advisory Committee for Aeronautics, 1953), also by T. C. Lin and R. E. Street (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Effect of variations in moments of inertia on spin and recovery characteristics of a single-engine low-wing monoplane with various tail arrangements including a twin tail (National Advisory Committee for Aeronautics, 1948), also by Anshal I. Neihouse (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of various missile characteristics on airframe frequency response (National Advisory Committee for Aeronautics, 1952), also by Howard F. Matthews, Walter E. McNeill, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of vertical-tail area and length on the yawing stability characteristics of a model having a 45° sweptback wing (National Advisory Committee for Aeronautics, 1951), also by William Letko (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effect of wall friction on the strength of shock waves in tubes and hydraulic jumps in channels (National Advisory Committee for Aeronautics, 1949), also by Coleman duP. Donaldson and Roger D. Sullivan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effect of yaw and angle of attack on pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71 (National Advisory Committee for Aeronautics, 1954), also by Raymond J. Comenzo, Ernest A. Mackley, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60° delta wing at Mach numbers from 0.75 to 1.96 (National Advisory Committee for Aeronautics, 1955), also by Lawrence D. Guy and Hoyt V. Brown (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60 (National Advisory Committee for Aeronautics, 1949), also by F. E. West and T. Himka (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of compressibility on the performance of two full-scale helicopter rotors (National Advisory Committee for Aeronautics, 1951), also by Paul J. Carpenter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effects of compressibility on the upwash at the propeller planes of a four-engine tractor airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10 (National Advisory Committee for Aeronautics, 1953), also by Armando E. Lopez, Jerald K. Dickson, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions (National Advisory Committee for Aeronautics, 1948), also by Ralph T. Dittrich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections (National Advisory Committee for Aeronautics, 1950), also by G. Chester Furlong and James E. Fitzpatrick (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effects of mass distribution on the low-speed dynamic lateral stability and control characteristics of a model with a 45° sweptback wing (National Advisory Committee for Aeronautics, 1951), also by Donald E. Hewes (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of multiaxial stretching on crazing and other properties of transparant plastics (National Advisory Committee for Aeronautics, 1954), also by Irvin Wolock and Desmond Ivan George (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Lawrence D. Guy and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effects of powered controls and fire-control systems on tracking accuracy (National Advisory Committee for Aeronautics, 1955), also by George A. Rathert, Burnett L. Gadeberg, Marvin Abramovitz, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effects of sideslip, aspect ratio, and Mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Arthur L. Jones, Elizabeth E. Lindler, and Robert M. Sorenson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4 (National Advisory Committee for Aeronautics, 1954), also by Homer P. Mason, Allen B. Henning, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of some solution treatments followed by an aging treatment on the life of small cast gas-turbine blades of a cobalt-chromium-base alloy. [Part] 1, Effect of solution-treating temperature (National Advisory Committee for Aeronautics, 1951), also by C. Yaker and C. A. Hoffman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of special leading- and trailing-edge modifications on blade temperature (National Advisory Committee for Aeronautics, 1951), also by Herman H. Ellerbrock, Gordon T. Smith, Charles F. Zalabak, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of sting-support interference on the drag of an ogive-cylinder body with and without a boattail at 0.6 to 1.4 mach number (National Advisory Committee for Aeronautics, 1957), also by George Lee, James L. Summers, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds (National Advisory Committee for Aeronautics, 1956), also by John P. Mugler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds (National Advisory Committee for Aeronautics, 1956), also by Frank S. Malvestuto, William J. Alford, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3 (National Advisory Committee for Aeronautics, 1957), also by Allen B. Henning (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model (National Advisory Committee for Aeronautics, 1954), also by Alex Goodman and David F. Thomas (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model (National Advisory Committee for Aeronautics, 1957), also by Powell M. Lovell, Lysle P. Parlett, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4 (National Advisory Committee for Aeronautics, 1957), also by Earl D. Knechtel, George Lee, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Effects on adjacent surfaces from the firing of rocket jets (National Advisory Committee for Aeronautics, 1957), also by Walter E. Bressette, Abraham Leiss, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives (National Advisory Committee for Aeronautics, 1952), also by Robert O. Schade and James L. Hassell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Efficiency of radial-flow turbine of turbo engineering corporation TT13-18 turbo super charger (National Advisory Committee for Aeronautics, 1947), also by Earl E. Coulter, William R. Galloway, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The elasto-plastic stability of plates (NACA, 1947), also by A. A. Il§i�ushin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Elevated-temperature combined stress-rupture plus fatigue strength of waspaloy having having different aging treatments and/or molybedenum contents (National Advisory Committee for Aeronautics, 1958), also by Charles A. Hoffman, M. B. Hornak, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Elevated-temperature compressive stress-strain data for 24S-T3 aluminum-alloy sheet and comparisons with extruded 75S-T6 aluminum alloy (National Advisory Committee for Aeronautics, 1949), also by William M. Roberts (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Elevated-temperature fatigue properties of two titanium alloys (National Advisory Committee for Aeronautics, 1956), also by William K. Rey (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Elevated-temperature properties of several titanium carbide base ceramals (National Advisory Committee for Aeronautics, 1949), also by George C. Deutsch, William G. Lidman, and Andrew J. Repko (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The elliptic wing based on the potential theory (NACA, 1941), also by Klaus Krienes (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Endurance evaluation of several tube-filled rotor blades (National Advisory Committee for Aeronautics, 1952), also by Jack B. Esgar, John L. Clure, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Endurance evaluation of shell-supported turbine rotor blades made of timken 17-22A (S) steel (National Advisory Committee for Aeronautics, 1951), also by Francis S. Stepka, John L. Clure, H. Robert Bear, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Engine design-point performance (National Advisory Committee for Aeronautics, 1954), also by James E. Hubbartt, Wilson B. Schramm, R. J. Rossbach, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the Mach lines (National Advisory Committee for Aeronautics, 1950), also by Kennith L. Goin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis (National Advisory Committee for Aeronautics, 1949), also by John C. Sanders and Edward C. Chapin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Estimates of probability distribution of root-mean-square gust velocity of atmospheric turbulence from operational gust-load data by random-process theory (National Advisory Committee for Aeronautics, 1955), also by Harry Press, Ivan Hadlock, and May T. Meadows (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Estimation of the damping in roll of rings through the normal flight range of lift coefficient (National Advisory Committee for Aeronautics, 1949), also by Alex Goodman and Glenn H. Adair (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine (National Advisory Committee for Aeronautics, 1954), also by C. R. Morse and R. H. Kemp (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Evaluation of five conical center-body supersonic diffusers at several angles of attack (National Advisory Committee for Aeronautics, 1952), also by Gerald W. Englert, Leonard J. Obery, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Evaluation of packed distillation columns. [Part] 1, Atmospheric pressure (National Advisory Committee for Aeronautics, 1951), also by Thaine W. Reynolds and George H. Sugimura (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Evaluation of proposed reference fuel scales for knock rating (National Advisory Committee for Aeronautics, 1948), also by Henry C. Barnett and Thomas C. Clarke (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Evaluation of the use of electrical resistance for detecting overtemperatured S-816 turbine blades (National Advisory Committee for Aeronautics, 1957), also by Leonard Robins, Lewis A. Rodert, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An evaluation of the use of ground radar for avoiding severe turbulence associated with thunderstorms (National Advisory Committee for Aeronautics, 1949), also by J. K. Thompson and V. W. Lipscomb (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An evaluation of two cooling-air ejectors in flight at transonic speeds (National Advisory Committee for Aeronautics, 1954), also by L. Stewart Rolls, C. Dewey Havill, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature (National Advisory Committee for Aeronautics, 1954), also by Patrick L. Donoughe and John N. B. Livingood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Examination of smoke and carbon from turbojet-engine combustors (National Advisory Committee for Aeronautics, 1952), also by Thomas P. Clark and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The excitation of unstable perturbations (NACA, 1952), also by J. Pretsch (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow (National Advisory Committee for Aeronautics, 1951), also by Robert L. Halfman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination (Washington, D.C. : National Advisory Committee for Aeronautics, [1955], 1955), also by William J. Alford, Thomas J. King, H. Norman Silvers, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental and predicted lateral-directional dynamic-response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet (National Advisory Committee for Aeronautics, 1956), also by Stuart C. Brown and Euclid C. Holleman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet (National Advisory Committee for Aeronautics, 1954), also by Henry A. Jr Cole, Euclid C. Holleman, Stuart C. Brown, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental and theoretical determination of thermal stresses in a flat plate (National Advisory Committee for Aeronautics, 1952), also by Richard R. Heldenfels, William M. Roberts, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental and theoretical distribution of flow produced by inlet guide vanes of an axial-flow compressor (National Advisory Committee for Aeronautics, 1949), also by Harold B. Finger, Howard A. Buckner, and Harold J. Schum (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental and theoretical investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic characteristics in sideslip of an unswept, untapered tail assembly (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Harleth G. Wiley, Donald R. Riley, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental cooling-air impeller performance and turbine rotor temperatures in modified J33 split-disk rotor up to speeds of 10,000 RPM (National Advisory Committee for Aeronautics, 1952), also by Alfred J. Nachtigall, Robert R. Ziemer, Charles F. Zalabak, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers (National Advisory Committee for Aeronautics, 1957), also by John A. Moore, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental determination of local and mean coefficients of heat transfer for turbulent flow in pipes (NACA, 1954), also by I. T. Aladyev (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates (NACA, 1954), also by Eldon W. Sams, Walter F. Weiland, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations (NACA, 1955), also by Harry W. Carlson, John P. Gapcynski, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of a lightweight rocket chamber (National Advisory Committee for Aeronautics, 1953), also by John E. Dalgleish, Adelbert O. Tischler, and Lewis Flilght Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications (NACA, 1952), also by Patrick L. Donoughe, Roy A. McKinnon, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities (National Advisory Committee for Aeronautics, 1952), also by Dean R. Chapman, Robert H. Kester, and William R. Wimbrow (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of creep bending and buckling of thin circular cylindrical shells (National Advisory Committee for Aeronautics, 1957), also by Burton Erickson (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of external water-spray cooling in a turbojet engine utilizing several injection configurations including orifices in the rotor-blade bases (National Advisory Committee for Aeronautics, 1955), also by Roy A. McKinnon, John C. Freche, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients (National Advisory Committee for Aeronautics, 1952), also by Loren A. Beatty, James C. Emery, Melvyn Savage, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of free-convection heat transfer in vertical tube at large grashof numbers (National Advisory Committee for Aeronautics, 1952), also by E. R. G. Eckert, A. J. Diagula, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design (National Advisory Committee for Aeronautics, 1953), also by Hubert W. Allen, Richard E. Chamness, and Milton G. Kofskey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of NACA submerged air inlets on a one fifth scale model of a fighter airplane. (National Advisory Committee for Aeronautics, 1947), also by Donald E. Gault and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental investigation of regions of separated laminar flow (NACA, 1955), also by Donald E. Gault (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds (National Advisory Committee for Aeronautics, 1949), also by William R. Wimbrow (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental investigation of the design variables for NACA submerged duct entrances (National Advisory Committee for Aeronautics, 1948), also by Emmet A. Mossman and Lauros M. Randall (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow (National Advisory Committee for Aeronautics, 1951), also by Robert W. Higgins and Constantine C. Pappas (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5 (National Advisory Committee for Aeronautics, 1951), also by Edward W. Perkins (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number of 1.5 (NACA, 1947), also by Dean R. Chapman, Edward W. Perkins, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade (National Advisory Committee for Aeronautics, 1952), also by Louis J. Jr Schafer, Hadley T. Richards, Edward R. Bartoo, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental investigation of the normal acceleration of an airplane model in a gust (National Advisory Committee for Aeronautics, 1939), also by Philip Donely (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental investigation of the simulation of atmospheric entry of ballistic missiles (National Advisory Committee for Aeronautics, 1957), also by Stanford E. Neice, Bernard E. Cunningham, James A. Carson, and Ames Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer (National Advisory Committee for Aeronautics, 1951), also by Arthur E. Bryson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental pressure distributions over two wing-body combinations at Mach number 1.9 (NACA, 1951), also by Barry Moskowitz, Stephen H. Maslen, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Robert R. Howell, Albert L. Braslow, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental study of flow past turbine blades (NACA, 1949), also by E. Eckert, K. von Vietinghoff-Scheel, and J. Vanier (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experimental techniques for predicting store motions during release or ejection (National Advisory Committee for Aeronautics, 1959), also by Maxime A. Faget and Harry W. Carlson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experiments on stability of Bunsen-burner flames for turbulent flow (National Advisory Committee for Aeronautics ;, 1947), also by Lowell M. Bollinger and David T. Williams (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experiments with a model water tunnel (National Advisory Committee for Aeronautics ;, 1930), also by Eastman N. Jacobs, Ira H. Abbott, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment (National Advisory Committee for Aeronautics ;, 1931), also by I. H. Abbott (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Exploratory investigation of transpiration cooling of a 40À double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295À to 2,910À F (NACA, 1957), also by Bernard Rashis and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Exposure tests of galvanized-steel-stitched aluminum alloys (National Advisory Committee for Aeronautics, 1951), also by Fred M. Reinhart (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Extended applications of the hot-wire anemometer (National Advisory Committee for Aeronautics, 1949), also by Stanley Corrsin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Extension of the theory of oscillating airfoils of finite span in subsonic compressible flow (National Advisory Committee for Aeronautics, 1951), also by Eric Reissner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Extension to the cases of two dimensional and spherically symmetric flows of two particular solutions to the equations of motion governing unsteady flow in a gas (NACA, 1952), also by Lorenzo Poggi (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Factors affecting the maximum lift-drag ratio at high supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Charles H. McLellan, Robert W. Dunning, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Factors affecting transition at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Archibald R. Sinclair, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Fatigue testing machine for applying a sequence of loads of two amplitudes (National Advisory Committee for Aeronautics, 1951), also by Richard Barksdale Harwell, Ira Smith, Darnley M. Howard, and Frank C. Smith (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Finite span wings in compressible flow (NACA, 1956), also by E. A. Krasil§shchikova (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flat plate cascades at supersonic speed (NACA, 1956), also by Rashad M. El Badrawy (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A flat wing with sharp edges in a supersonic stream (NACA, 1956), also by A. E. Donov (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers (National Advisory Committee for Aeronautics, 1956), also by Charles W. Mathews, Howard C. Kyle, and Donald C. Cheatham (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight and analytical study of roll requirements of a fighter airplane (National Advisory Committee for Aeronautics, 1956), also by James J. Adams (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8 (National Advisory Committee for Aeronautics, 1956), also by Leonard W. Putland, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight determination of drag of normal-shock nose inlets with various cowling profiles at mach numbers from 0.9 to 1.5 (U.S. Government Printing Office, 1956), also by R. I. Sears, L. W. Putland, and C. F. Merlet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8 (National Advisory Committee for Aeronautics, 1951), also by R. I. Sears, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane (National Advisory Committee for Aeronautics, 1949), also by Charles J. Liddell, Donovan R. Heinle, and Rudolph D. Van Dyke (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift (National Advisory Committee for Aeronautics, 1950), also by John D. Morrow, Ellis Katz, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane (National Advisory Committee for Aeronautics, 1951), also by B. Porter Brown, James B. Whitten, and Robert G. Chilton (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1 (National Advisory Committee for Aeronautics, 1957), also by Walter A. Bartlett, Charles F. Merlet, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane (National Advisory Committee for Aeronautics, 1957), also by S. A. Sjoberg, William L. Alford, and Walter R. Russell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of a supersonic canard missile equipped with an auxiliary damping-in-pitch control system (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Martin T. Moul and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of an aileron and a spoiler on a wing of the X-3 airplane plan form at Mach numbers from 0.5 to 1.6 (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Roland D. English and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane (National Advisory Committee for Aeronautics, 1951), also by James B. Whitten, Donald E. Hewes, Paul A. Hunter, and John P. Campbell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A flight investigation of the effects of compressibility on applied gust loads (National Advisory Committee for Aeronautics, 1949), also by E. T. Binckley and Jack Funk (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight investigation of the variation of static-pressure error of a static-pressure tube with distance ahead of a wing and a fuselage (National Advisory Committee for Aeronautics, 1951), also by William Gracey and Elwood F. Scheithauer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight measurements of aerodynamic loads on the horizontal tail surface of a fighter-type airplane (National Advisory Committee for Aeronautics, 1947), also by John B. Garvin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight measurements of airplane structural temperatures at supersonic speeds (NACA, 1957), also by Richard D. Banner and Flight Research Center (U.S.) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight measurements of the flying qualities of five light airplanes (National Advisory Committee for Aeronautics, 1948), also by Paul A. Hunter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight techniques for determining airplane drag at high Mach numbers (National Advisory Committee for Aeronautics, 1956), also by De E. Beeler, Edwin J. Saltzman, and Donald R. Bellman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree swept-back wing. (National Advisory Committee for Aeronautics, 1955), also by Richard S. Bray, Robert C. Innis, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight tests of experimental beveled-trailing-edge Frise ailerons on a fighter airplane (National Advisory Committee for Aeronautics ;, 1946), also by R. Fabian Goranson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flight tests of the hydrodynamic characteristics of a Japanese "Emily" flying boat (National Advisory Committee for Aeronautics, 1949), also by J. A. Ferguson, R. J. Corber, and R. E. Seibels (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane (National Advisory Committee for Aeronautics, 1951), also by William Bihrle (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flow of gas through turbine lattices (Langley Memorial Aeronautical Laboratory, 1956), also by M. E. Deĭch and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The flow of gases in narrow channels (NACA, 1951), also by R. E. H. Rasmussen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flow over a slender body of revolution at supersonic velocities (National Advisory Committee for Aeronautics ;, 1946), also by Robert T. Jones and Kenneth Margolis (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 (NACA, 1954), also by W. F. Lindsey and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flow through cascades in tandem (National Advisory Committee for Aeronautics, 1951), also by William E. Spraglin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Fluctuations in a spray formed by two impinging jets (National Advisory Committee for Aeronautics, 1951), also by Marcus F. Heidmann and Jack C. Humphrey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flutter at very high speeds (National Advisory Committee for Aeronautics, 1957), also by Harry L. Runyan, Homer G. Morgan, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model (National Advisory Committee for Aeronautics, 1956), also by Albert P. Martina, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. [Part] 2, Isentropic-spike all-external compression inlet (National Advisory Committee for Aeronautics, 1951), also by L. J. Obery, G. W. Englert, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Formation of a vortex at the edge of a plate (NACA, 1956), also by Leo Anton (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Formulas and tables of coefficients for numerical differentiation with function values given at unequally spaced points and application to solution of partial differential equations (National Advisory Committee for Aeronautics, 1950), also by Zhonghua Wu and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Free fall and evaporation of n-octane droplets in the atmosphere as applied to the jettisoning of aviation gasoline at altitude (National Advisory Committee for Aeronautics, 1953), also by Herman H. Lowell and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50 (National Advisory Committee for Aeronautics, 1955), also by Ralph A. Falanga, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration (National Advisory Committee for Aeronautics, 1955), also by Charles B. Rumsey, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4 (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Eugene D. Schult, E. M. Fields, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Free-space oscillating pressures near the tips of rotating propellers (National Advisory Committee for Aeronautics, 1949), also by Harvey H. Hubbard and Arthur A. Regier (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Friction of solid films on steel at high sliding velocities (National Advisory Committee for Aeronautics, 1948), also by Robert L. Johnson, E. E. Bisson, and Douglas Godfrey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Friction, wear, and surface damage of metals as affected by solid surface films (National Advisory Committee for Aeronautics, 1955), also by Douglas Godfrey, Max A. Swikert, Robert L. Johnson, and E. E. Bisson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: From linear mechanics to nonlinear mechanics (NACA, 1955), also by Julien Loeb (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Fundamental effects of aging on creep properties of solution-treated low-carbon N-155 alloy (National Advisory Committee for Aeronautics, 1949), also by D. N. Frey, A. E. White, and J. W. Freeman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Further experiments on the flow and heat transfer in a heated turbulent air jet (National Advisory Committee for Aeronautics, 1949), also by Stanley Corrsin and M. S. Uberoi (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Further measurements of normal accelerations on racing airplanes (National Advisory Committee for Aeronautics, 1936), also by Nathan F. Scudder and H. W. Kirshbaum (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Further study of metal transfer between sliding surfaces (National Advisory Committee for Aeronautics, 1951), also by J. T. Burwell and C. D. Strang (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Gas flow with straight transition line (NACA, 1951), also by L. V. Ovsi�annikov (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Gas motion in a local supersonic region and conditions of potential-flow breakdown (NACA, 1949), also by A. A. Nikol§skiĭ and G. I. Taganov (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Gaskinetik sehr hoher fluggeschwindigkeiten (National Advisory Committee for Aeronautics, 1950), also by Eugen Sanger (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: General algebraic method applied to control analysis of complex engine types (National Advisory Committee for Aeronautics, 1949), also by Aaron S. Boksenbom and Richard Hood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: General characteristics of the flow through nozzles at near critical speeds (NACA, 1947), also by R. Sauer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: General potential theory of arbitrary wing sections (Government Printing Office, 1933), also by T. Theodorsen and I. E. Garrick (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: General solutions of optimum problems in nonstationary flight (NACA, 1955), also by Angelo Miele and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: General theory of conical flows and its application to supersonic aerodynamics (NACA, 1955), also by Paul Germain (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations (National Advisory Committee for Aeronautics, 1955), also by Jack N. Nielsen and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system (National Advisory Committee for Aeronautics, 1951), also by Artur Mager (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities (NACA, 1951), also by L. G. Loĭt�si�anskiĭ (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Generalization of turbojet-engine performance in terms of pumping characteristics (National Advisory Committee for Aeronautics, 1949), also by Newell D. Sanders and Michael Behun (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Generalized analysis of experimental observations in problems of elastic stability (National Advisory Committee for Aeronautics, 1938), also by Eugene E. Lundquist (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A glimpse of scientific research on fundamental problems of military and civil aeronautics ... ([U. S. Govt. print. off.], 1939) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A glimpse of scientific research on fundamental problems of military and civil aircraft ... ([U.S. G.P.O.], 1936) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A glimpse of scientific research on fundamental problems of military and civil aircraft ... ([U.S. Govt. Print. Off], 1935) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Grenzschichten in flüssigkeiten mit kleiner reibung (National Advisory Committee for Aeronautics, 1950), also by H. Blasius (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Growth of disturbances in a flame-generated shear region (National Advisory Committee for Aeronautics, 1956), also by Perry L. Blackshear (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Gust-tunnel investigation of a flexible-wing model with semichord line swept back 45° (National Advisory Committee for Aeronautics, 1949), also by Thomas D. Reisert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat, mass, and momentum transfer for flow over a flat plate with blowing or suction (National Advisory Committee for Aeronautics, 1954), also by H. S. Mickley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0 (National Advisory Committee for Aeronautics, 1958), also by J. Thomas Markley, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds (NACA, 1952), also by Coleman duP. Donaldson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat-transfer characteristics of blunt 2 and 3 dimensional bodies at supersonic speeds. (National Advisory Committee for Aeronautics, 1956), also by Glen Goodwin and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transfer, diffusion and evaporation (NACA, 1954), also by Wilhelm Nusselt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transfer from high-temperature surfaces to fluids. [Part] 1, Preliminary investigation with air in inconel tube with rounded entrance, inside diameter of 0.4 inch and length of 24 inches (National Advisory Committee for Aeronautics, 1948), also by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transfer on an afterbody immersed in the separated wake of a hemisphere (National Advisory Committee for Aeronautics, 1958), also by Helmer V. Nielsen and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by John O. Jr Reller and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Heat transmission in the boundary layer (NACA, 1949), also by L. E. |q Kalikhman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: High-altitude flight cooling investigation of a radial air-cooled engine (National Advisory Committee for Aeronautics ;, 1946), also by Eugene J. Manganiello, E. Barton Bell, and Michael F. Valerino (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging (National Advisory Committee for Aeronautics, 1954), also by Wilfred E. Scull and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: High-resolution autoradiography (National Advisory Committee for Aeronautics, 1954), also by George C. Towe, J. W. Freeman, and Henry J. Gomberg (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: High-temperature protection of a titanium-carbide ceramal with a ceramic-metal coating having a high chromium content (National Advisory Committee for Aeronautics, 1951), also by Dwight G. Moore, William N. Harrison, and Stanley G. Benner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Hydrocarbon and nonhydrocarbon derivatives of cyclopropane : errata no. 1 (U.S. G.P.O., 1953), also by Simon Ostrach, Louis C. Gibbons, and Paul H. Wise (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The hydrodynamic characteristics of an aspect-ratio-0.125 modified rectangular flat plate operating near a free water surface (National Advisory Committee for Aeronautics, 1954), also by John A. Ramsen and Victor L. Vaughan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Hydrodynamic properties of planing surfaces and flying boats (NACA, 1950), also by N. A. Sokolov (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Ignition-delay characteristics in modified open-cup apparatus of several fuels with nitric acid oxidants within temperature range 70 degrees to 105 degrees F (National Advisory Committee for Aeronautics, 1951), also by Riley O. Miller and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Improvement of accuracy of balanced-pressure indicators and development of an indicator calibrating machine (National Advisory Committee for Aeronautics, 1949), also by James C. Livengood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Increasing the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling (National Advisory Committee for Aeronautics ;, 1946), also by George J. Heimerl and Walter Woods (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Index of aircraft materials research reports. (Washington, 1947) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Index of NACA technical publications (NACA, 1947), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Infiltration of titanium carbide with several metals (National Advisory Committee for Aeronautics, 1952), also by Raymond S. Gurnick, Anthony L. Cooper, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Infinitesimal conical supersonic flow (NACA, 1947), also by Adolf Busemann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Influence of alloying upon grain-boundary creep (National Advisory Committee for Aeronautics, 1956), also by F. N. Rhines, M. A. Kissel, and W. E. Bond (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Influence of external variables on smoking of benzene flames (National Advisory Committee for Aeronautics, 1952), also by Thomas P. Clark and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Influence of hot-working conditions on high-temperature properties of a heat-resistant alloy (U.S. Government Printing Office, 1957), also by John F. Ewing and J. W. Freeman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Influence of large amounts of wing sweep on stability and control problems of aircraft (National Advisory Committee for Aeronautics ;, 1946), also by Hartley A. Soule (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule (National Advisory Committee for Aeronautics, 1956), also by William A. Page and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The influence of the form of a wooden beam on its stiffness and strength. I, Deflection of beams with special reference to shear deformations (Government Printing Office, 1923), also by J. A. Newlin and G. W. Trayer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin (National Advisory Committee for Aeronautics, 1948), also by Ralph W. Stone and Walter J. Klinar (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Influence of wall boundary layer upon the performance of an axial-flow fan rotor (National Advisory Committee for Aeronautics, 1951), also by Emanuel Boxer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region (National Advisory Committee for Aeronautics, 1955), also by Harold B. Pierce, Thomas D. Reisert, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Initial investigation of carbide-type ceramal of 80-percent titanium carbide plus 20-percent cobalt for use as gas-turbine-blade material (National Advisory Committee for Aeronautics, 1949), also by Charles A. Hoffman and G. Mervin Ault (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Initial results of instrument-flying trials conducted in a single-rotor helicopter (National Advisory Committee for Aeronautics, 1952), also by Almer D. Crim, James B. Whitten, and John P. Reeder (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An inlet design concept to reduce flow distortion at angle of attack (National Advisory Committee for Aeronautics, 1957), also by Carl F. Schueller, Leonard E. Stitt, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Instrumentation of the ames supersonic free-flight wind tunnel (National Advisory Committee for Aeronautics, 1952), also by Robert O. Briggs, Stanley F. Schmidt, William J. Kerwin, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Integrating manometer for use in wind tunnel pressure distribution measurements (National Advisory Committee for Aeronautics ;, 1931), also by Richard W. Noyes (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet (National Advisory Committee for Aeronautics, 1955), also by James C. Laurence (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Interaction of moving shocks and hot layers (National Advisory Committee for Aeronautics, 1957), also by Robert V. Hess and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Interference effects and drag of struts on a monoplae wing (National Advisory Committee for Aeronautics ;, 1931), also by Kenneth E. Ward (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics (National Advisory Committee for Aeronautics, 1956), also by H. George Krull, William T. Beale, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Introduction to electrical-circuit analogies for beam analysis (National Advisory Committee for Aeronautics, 1952), also by Stanley U. Benscoter and Richard H. MacNeal (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45° sweptback highly tapered wing in combination with basic and indented bodies (National Advisory Committee for Aeronautics, 1957), also by Thomas L. Fischetti, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles (National Advisory Committee for Aeronautics, 1956), also by Donald P. Hearth, Robert W. Cubbison, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination (National Advisory Committee for Aeronautics, 1958), also by J. Cary Nettles, Robert C. Campbell, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47° sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel (National Advisory Committee for Aeronautics, 1951), also by Ralph P. Bielat, Domenic A. Coppolino, and Daniel E. Harrison (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by William C. Moseley and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), also by Jack F. Runckel, Edwin E.. Jr Lee, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps (National Advisory Committee for Aeronautics, 1948), also by James C. Sivells and Stanley H. Spooner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of 75-millimeter-bore cylindrical-roller bearings at high speeds. [Part] III, Lubrication and cooling studies - oil inlet distribution, oil inlet temperature, and generalized single-oil-jet cooling-correlation analysis (National Advisory Committee for Aeronautics, 1951), also by E. Fred Macks and Zolton N. Nemeth (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades (National Advisory Committee for Aeronautics, 1948), also by John C. Freche, Bob W. Sheflin, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of a simple device for preventing separation due to shock and boundary-layer interaction (National Advisory Committee for Aeronautics, 1950), also by Coleman duP. Donaldson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 (National Advisory Committee for Aeronautics, 1954), also by George C. Kenyon, Robert M. Reynolds, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of acceleration characteristics of a single-spool turbojet engine (National Advisory Committee for Aeronautics, 1953), also by Frank L. Oppenheimer, George J. Pack, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Investigation of aircraft heaters. XXXII - Measurement of thermal conductivity of air and of exhaust gases between 50©� and 900©� F. (National Advisory Committee for Aeronautics, 1949), also by L. M. K. Boelter and W. H. Sharp (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air (National Advisory Committee for Aeronautics, 1957), also by James F. Connors, Rudolph C. Meyer, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of axially symmetric and two-dimensional multinozzles for producing supersonic streams (National Advisory Committee for Aeronautics, 1952), also by Eli Reshotko, Rudolph C. Haefeli, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of bonding between metals and ceramics. [Part] 1, Nickel, cobalt, iron or chromium with boron carbide (National Advisory Committee for Aeronautics, 1949), also by H. J. Hamjian and W. G. Lidman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of combustion screech and a method of its control (National Advisory Committee for Aeronautics, 1954), also by James L. Jr Harp, Lively Bryant, Wallace W. Velie, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of effect of notches on elevated-temperature fatigue strength of N-155 alloy (National Advisory Committee for Aeronautics, 1954), also by C. A. Hoffman (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Investigation of effects of reynolds number on large double-entry centrifugal compressor (National Advisory Committee for Aeronautics, 1952), also by Karl Kovach, Joseph R. Withee, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds (National Advisory Committee for Aeronautics, 1958), also by Abraham Leiss, Walter J. Kouyoumjian, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of influence of chemical composition on forged modified low-carbon N-155 alloys in solution-treated and aged condition as related to rupture properties at 1200° F (National Advisory Committee for Aeronautics, 1951), also by E. E. Reynolds, A. E. White, and J. W. Freeman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Investigation of pure bending in the plastic range when loads are not parallel to a principal plane (National Advisory Committee for Aeronautics, 1951), also by Harry A. Williams (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of Reynolds number effects for a series of cone-cylinder bodies at Mach number of 1.62, 1.93, and 2.41 (NACA, 1953), also by Carl E. Grigsby and Edmund L. Ogburn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition (U.S. Government Printing Office, 1958), also by Dean R. Chapman, Howard K. Larson, and Donald M. Kuehn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of separation of the turbulent boundary layer (National Advisory Committee for Aeronautics, 1950), also by G. B. Schubauer and P. S. Klebanoff (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2 (National Advisory Committee for Aeronautics, 1950), also by Robert E. Pendley, Harold L. Robinson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Investigation of sheet-stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners (National Advisory Committee for Aeronautics, 1940), also by Louis Dunn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps (National Advisory Committee for Aeronautics, 1949), also by Jack Fischel and James M. Watson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord (National Advisory Committee for Aeronautics, 1954), also by Mitchel H. Bertram, William D. McCauley, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the aerodynamic characteristics in pitch and sideslip of a 45° swept-wing airplane configuration with various vertical locations of the wing and horizontal tail. Static lateral and directional stability ; Mach numbers of 1.41 and 2.01 (National Advisory Committee for Aeronautics, 1957), also by M. Leroy Spearman, Ross B. Robinson, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90° (National Advisory Committee for Aeronautics, 1954), also by John W. Draper and Richard E. Kuhn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An investigation of the creep lifetime of 75S-T6 aluminum-alloy columns (National Advisory Committee for Aeronautics, 1954), also by Eldon E. Mathauser and William A. Brooks (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the discharge rate of a fuel-injection system (National Advisory Committee for Aeronautics ;, 1931), also by Harold C. Gerrish and Fred Voss (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the effect of a tip modification and thermal de-icing air flow on propeller performance (National Advisory Committee for Aeronautics ;, 1946), also by Blake W. Corson and Julian D. Maynard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45° sweptback wing-body configuration at transonic speeds (National Advisory Committee for Aeronautics, 1954), also by Claude V. Williams, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45° sweptback wing of aspect ratio 4 (National Advisory Committee for Aeronautics, 1957), also by Kenneth P. Spreemann, William J. Alford, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), also by Archibald E. Morse, Ulysse J. Blanchard, David R. Woodward, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925 (National Advisory Committee for Aeronautics, 1949), also by James B. Delano, Francis G. Morgan, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925 (National Advisory Committee for Aeronautics, 1949), also by James B. Delano, Daniel E. Harrison, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the penetration of an air jet directed perpendicularly to an air stream (National Advisory Committee for Aeronautics, 1948), also by Edmund E. Callaghan and Robert S. Ruggeri (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot (National Advisory Committee for Aeronautics, 1950), also by Robert A. Gardiner, H. O. Ankenbruck, and Jacob Zarovsky (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of the stability of the laminar boundary layer in a compressible fluid (National Advisory Committee for Aeronautics ;, 1946), also by Lester Lees and C. C. Lin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74 (National Advisory Committee for Aeronautics, 1951), also by L. Eugene Baughman, Larence I. Gould, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6 (National Advisory Committee for Aeronautics, 1957), also by George W. Jones, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of transonic turbine designed for zero diffusion of suction-surface velocity (National Advisory Committee for Aeronautics, 1954), also by Warren J. Whitney, R. Y. Wong, Daniel E. Monroe, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of turbulent flow in a two-dimensional channel (National Advisory Committee for Aeronautics, 1950), also by John Laufer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5. [Part] I, , Velocity-diagram study (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, Warner L. Stewart, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation toward simplification of missile control systems (National Advisory Committee for Aeronautics, 1953), also by Howard J. Curfman, Harold L. Crane, H. Kurt Strass, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigation with an interferometer of the turbulent mixing of a free supersonic jet (National Advisory Committee for Aeronautics, 1949), also by Paul B. Gooderum, Maurice J. Brevoort, and George P. Wood (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles (National Advisory Committee for Aeronautics, 1949), also by Eugene S. Love, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigations of the boundary-layer control on a full scale swept wing with air bled off from the turbojet (NACA, 1952), also by Pierre Rebuffet and Ph. Poisson-Quinton (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Investigations on reductions of friction on wings, in particular by means of boundary layer suction (NACA, 1947), also by Werner Pfenninger (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Isolated and cascade airfoils with prescribed velocity distribution (National Advisory Committee for Aeronautics, 1947), also by John M. Riebs and Meyer Jerison (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: An Iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems (National Advisory Committee for Aeronautics, 1951), also by Myron L. Gossard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Jet diffuser for simulating ram conditions on a turbojet-engine static test stand (National Advisory Committee for Aeronautics, 1947), also by Robert H. Essig, David S. Gabriel, H. R. Bohanon, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Jet diffusion in proximity of a wall (NACA, 1949), also by D. Küchemann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Robert F. Peck and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: K voprosu o povedenii bystrodvizhushchegosya potoka szhimaemogo gaza v pryamoi tsilindricheskoi trube pri nalichii okhlazhdenia (National Advisory Committee for Aeronautics, 1951), also by G. A. Varshavsky (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Kinetic treatment of the nucleation in supersaturated vapors (NACA, 1954), also by R. Becker and Werner Döring (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Knock-limited performance of fuel blends containing aromatics. [Part] 6, 10 Alkylbenzenes (National Advisory Committee for Aeronautics, 1949), also by I. L. Drell and H. E. Alquist (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Knock-limited performance of several branched paraffins and olefins (National Advisory Committee for Aeronautics, 1948), also by R. S. Genco and I. L. Drell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Knocking combustion observed in a spark-ignition engine with simultaneous direct and schlieren high-speed motion pictures and pressure records (National Advisory Committee for Aeronautics, 1948), also by Gordon E. Osterstrom (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lame's wave functions of the ellipsoid of revolution (NACA, 1949), also by J. Meixner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Laminar flow about a rotating body of revolution in an axial airstream (NACA, 1956), also by H. Schlichting (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Laminar flow of a slightly viscous incompressible fluid that issues from a slit and passes over a flat plate (National Advisory Committee for Aeronautics, 1948), also by Neal Tetervin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Landing and taxiing tests over various types of runway lights (National Advisory Committee for Aeronautics, 1958), also by Robert C. Dreher and Sidney A. Batterson (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Landing conditions for large airplanes in routine operations (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Norman S. Silsby, Ezlaslav N. Harrin, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine (National Advisory Committee for Aeronautics ;, 1946), also by K. R. Czarnecki and Jerome Pasamanick (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Langley full-scale-tunnel tests of the custer channel wing airplane (NACA, 1953), also by Jerome Pasamanick and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35°, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1950), also by Robert F. Thompson, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lateral elastic instability of hat-section stringers under compressive load (National Advisory Committee for Aeronautics, 1951), also by Stanley Goodman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Lateral stability of equal-flanged aluminum-alloy I-beams subjected to pure bending (National Advisory Committee for Aeronautics ;, 1940), also by C. Dumont and H. N. Hill (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A least squares curve fitting method with applications to the calculation of stability coefficients from transient-response data (National Advisory Committee for Aeronautics, 1951), also by Marvin Shinbrot (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lecture series "boundary layer theory." Part II, turbulent flows (NACA, 1949), also by H. Schlichting (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift and drag characteristics of a cabin monoplane determined in flight (National Advisory Committee for Aeronautics ;, 1931), also by F. L. Thompson and P. H. Keister (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift and moment on oscillating triangular and related wings with supersonic edges (National Advisory Committee for Aeronautics, 1951), also by Herbert C. Nelson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift-curve slopes determined in flight on a flexible swept-wing jet bomber (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), also by William S. Aiken, Raymond A. Fisher, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by Harvard Lomax (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift hysteresis at stall as an unsteady boundary-layer phenomenon (U.S. Government Printing Office, 1956), also by F. K. Moore (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift on a bent, flat plate (NACA, 1952), also by F. Keune (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio (National Advisory Committee for Aeronautics, 1951), also by Edward J. Hopkins (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lightning discharges to aircraft and associated meteorological conditions (National Advisory Committee for Aeronautics, 1946), also by L. P. Harrison (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Limitations of the pilot in applying forces to airplane controls (National Advisory Committee for Aeronautics, 1936), also by Melvin N. Gough and A. P. Beard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Line-vortex theory for calculation of supersonic downwash (National Advisory Committee for Aeronautics, 1949), also by Harold Mirels and Rudolph C. Haefeli (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds (U.S. Government Printing Office, 1957), also by Percy J. Bobbitt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Linearized lifting-surface theory for swept-back wings with slender plan forms (National Advisory Committee for Aeronautics, 1949), also by Harvard Lomax and Max A. Heaslet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: List of NACA reports, 1947-1951. (Washington, 1953) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: List of NACA reports reprinted as Wartime reports. (National Advisory Committee for Aeronautics, 1948) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: List of NACA reports reprinted as Wartime reports. ([Washington, 1948) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: List of NACA wartime reports. ([Washington, 1948) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: List of reports with prices. (G.P.O., 1945) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: List of reports with prices (G.P.O., 1926) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: List of Technical notes, 1947-1953. (Washington, 1954) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lists of reports with prices ... (U. S. Govt. print. off., 1926) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Lo stato attuale delle ricerche sul moto instazionario di una superficie portante (National Advisory Committee for Aeronautics, 1951), also by P. Cicala (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Loads on external stores at transonic and supersonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Lawrence D. Guy and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Loads on thin wings at transonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Don D. Davis, Gerald Hieser, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Local isotropy in turbulent shear flow (National Advisory Committee for Aeronautics, 1958), also by Stanley Corrsin (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Location of detached shock wave in front of a body moving at supersonic speeds (National Advisory Committee for Aeronautics, 1947), also by Edmund V. Laitone and Otway O'M. Pardee (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone (National Advisory Committee for Aeronautics, 1954), also by Robert R. Hibbard, Wilfred E. Scull, Allen J. Metzler, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Low-speed experimental investigation of a thin, faired, double-wedge airfoil section with nose and trailing-edge flaps (National Advisory Committee for Aeronautics, 1949), also by Leonard M. Rose and John M. Altman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A low-speed investigation of a thin 60° delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size (National Advisory Committee for Aeronautics, 1955), also by Delwin R. Croom, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Low-speed static stability characteristics of a cambered-delta-wing model (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), also by John M. Riebe, William C. Moseley, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing (National Advisory Committee for Aeronautics, 1950), also by Arvid L. Keith, Jack Schiff, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Low-subsonic investigation to determine the chordwise pressure distribution and effectiveness of spoilers on a thin, low-aspect-ratio, unswept, untapered, semispan wing and on the wing with leading and trailing-edge flaps (National Advisory Committee for Aeronautics, 1958), also by Delwin R. Croom (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Lumped reflector parameters for two-group reactor calculations (National Advisory Committee for Aeronautics, 1952), also by Daniel Fieno, Robert B. Spooner, Harold Schneider, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Material presented at the NACA Conference on Compressor Research at Aircraft Engine Research Laboratory on September 11, 1946 (NACA, 1946), also by Ohio) NACA Conference on Compressor Research (1946 : Cleveland and Ohio) Aircraft Engine Research Laboratory (Cleveland (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Material presented at the NACA Conference on Supersonic Aerodynamics at Ames Aeronautical Laboratory on June 4, 1946, National Advisory Committee for Aeronautics. ([Washington?, 1946) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data (National Advisory Committee for Aeronautics, 1951), also by James J. Donegan and H. A. Pearson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurement and analysis of wing and tail buffeting loads on a fighter-type airplane (National Advisory Committee for Aeronautics, 1954), also by Wilber B. Huston and T. H. Skopinski (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures (NACA, 1954), also by Warren H. Lowdermilk, John N. B. Livingood, Walter F. Weiland, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurement of the longitudinal moment of inertia of a flexible airplane (National Advisory Committee for Aeronautics, 1956), also by Henry Ambrose Jr Cole, Frances L. Bennion, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurements and analysis of the motion of a canard airplane model in gusts (National Advisory Committee for Aeronautics, 1940), also by Philip Donely, Philip W. Pepoon, and Harold B. Pierce (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurements in the boundary layer of a yawed wing (National Advisory Committee for Aeronautics, 1949), also by A. M. Kuethe, W. H. Curry, and P. B. McKee (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 (NACA, 1956), also by Charles B. Rumsey, Dorothy B. Lee, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Measurements of runway roughness of four commercial airports (National Advisory Committee for Aeronautics, 1957), also by Dexter M. Potter (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Measurements of vertical air currents in the atmosphere (National Advisory Committee for Aeronautics, 1931), also by K. O. Lange and Joseph F. Vaniér (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Mechanical properties of pneumatic tires with special reference to modern aircraft tires (National Advisory Committee for Aeronautics, 1958), also by Robert F. Smiley, Walter B. Horne, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Mechanism of start and development of aircraft crash fires (National Advisory Committee for Aeronautics, 1952), also by I. Irving Pinkel, Gerard J. Pesman, and G. Merritt Preston (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Mechanisms of failure of high nickel-alloy turbojet combustion liners (National Advisory Committee for Aeronautics, 1949), also by John W. Weeton (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Metal-bonding adhesives for high-temperature service (National Advisory Committee for Aeronautics, 1955), also by John M. Black and Richard Frederick Blomquist (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Meteorology and aeronautics. (Govt. Printing Office., 1917) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Meteorology and aeronautics (Washington : Govt. Print. Off, 1917., 1917), also by William Richards Blair (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method and graphs for the evaluation of air-induction systems (U.S. Government Printing Office, 1953), also by George B. Brajnikoff (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds (National Advisory Committee for Aeronautics, 1951), also by Sidney M. Harmon (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method for calculating lift distribtutions for unswept wings with flaps or ailerons by use of nonlinear section lift data (National Advisory Committee for Aeronautics, 1951), also by James C. Sivells and Gertrude C. Westrick (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data (National Advisory Committee for Aeronautics, 1953), also by Albert P. Martina (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method for calculation of ram-jet performance (National Advisory Committee for Aeronautics, 1951), also by John R. Henry and J. Buel Bennett (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method for determining core dimensions of heat exchanger with one dominating film resistance and verification with experimental data (National Advisory Committee for Aeronautics, 1957), also by John N. B. Livingood, Anthony J. Diaguila, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method for determining distribution of luminous emitters in cone of laminar Bunsen flame (National Advisory Committee for Aeronautics, 1951), also by Thomas P. Clark (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Method for determining the aerodynamic characteristics of two- and three-dimensional shapes at hypersonic speeds (National Advisory Committee for Aeronautics, 1948), also by H. Reese Ivey, Edward N. Bowen, and E. Bernard Klunker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot (National Advisory Committee for Aeronautics, 1949), also by Robert T. Jones and Leonard Sternfield (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method for simulating the atmospheric entry of long-range ballistic missiles (NACA, 1955), also by A. J. Eggers and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method for studying helicopters longitudinal maneuver stability (National Advisory Committee for Aeronautics, 1953), also by Kenneth B. Amer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method of calculating a stability boundary that defines a region of satisfactory period-damping relationship of the oscillatory mode of motion (National Advisory Committee for Aeronautics, 1949), also by Leonard Sternfield and Ordway B. Gates (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method of calculating stresses in torsion-box covers with cutouts (National Advisory Committee for Aeronautics, 1951), also by Richard Rosecrans (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by use of accelerometer and attitude-angle measurements (National Advisory Committee for Aeronautics, 1950), also by John A. Zalovcik (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Method of designing airfoils with prescribed velocity distributions in compressible potential flows (National Advisory Committee for Aeronautics, 1949), also by George R. Costello (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A method of quadrature for calculation of the laminar and turbulent boundary layer in case of plane and rotationally symmetrical flow (NACA, 1955), also by Erich Truckenbrodt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Methods for connection to revolving thermocouples (National Advisory Committee for Aeronautics, 1951), also by Philip R. Tarr (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Methods for determining frequency response of engines and control systems from transient data (National Advisory Committee for Aeronautics, 1949), also by Melvin E. LaVerne and Aaron S. Boksenbom (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Methods of designing cascade blades with prescribed velocity distributions in compressible potential flows (National Advisory Committee for Aeronautics, 1949), also by George R. Costello (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The microstructure of turbulent flow (NACA, 1953), also by A. M. Obukhoff and A. M. I�Aglom (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Migration of cobalt during firing of ground-coat enamels on iron (National Advisory Committee for Aeronautics, 1952), also by William N. Harrison (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds (National Advisory Committee for Aeronautics, 1952), also by Paul E. Purser, Jesse L. Mitchell, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Model ditching investigation of a jet transport airplane with various engine installations (National Advisory Committee for Aeronautics, 1956), also by William C. Thompson (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution (National Advisory Committee for Aeronautics, 1951), also by David Graham (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Modified Wiener filter theory. (National Advisory Committee for Aeronautics, 1955), also by Elwood C. Stewart and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Moments of inertia of several airplanes (National Advisory Committee for Aeronautics ;, 1931), also by Marvel P. Miller and Hartley A. Soule (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA conference on aircraft power-plant controls; a compilation of the papers presented, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, November 17, 1948. ([Washington?, 1949) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Conference on Boundary Layers; a compilation of the papers presented, Langley Memorial Aeronautical Laboratory, Langley Field, Va., August 14, 1947. ([Washington?, 1947) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Conference on High-Speed Aerodynamics; a compilation of the papers presented, Amers Aeronautical Laboratory, Moffett Field, Calif., March 18, 19, and 20, 1958. ([Washington?, 1958) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA conference on some problems of aircraft operation [at] Lewis Flight Propulsion Laboratory, Cleveland, Ohio, November 17, 18, 1954. ([Washington?, 1955) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Conference on Turbine Cooling : a compilation of the papers presented by NACA staff members, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, November 9, 1949 (NACA, 1949), also by Ohio) NACA Conference on Turbine Cooling (1949 : Cleveland and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Conference on Turbine Materials and Cooling : a compilation of the papers presented, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, March 15, 1951 (NACA, 1951), also by Ohio) NACA Conference on Turbine Materials and Cooling (1951 : Cleveland and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Conference on Turbines : a compilation of papers presented by NACA staff members, Aircraft Engine Research Laboratory, Cleveland, Ohio, January 16, 1947 (National Advisory Committee for Aeronautics, 1947), also by Ohio) NACA Conference on Turbines (1947 : Cleveland and Ohio) Aircraft Engine Research Laboratory (Cleveland (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Conference on Turbojet-Engine Thrust-Augmentation Research; a compilation of the papers presented by NACA staff members, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, October 28, 1948. ([Washington?, 1948) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The NACA mixture analyzer and its application to mixture-distribution measurement in flight (National Advisory Committee for Aeronautics ;, 1947), also by Harold C. Gerrish (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA research abstracts and reclassification notice (National Advisory Committee for Aeronautics, 1956) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA research memorandum (Washington, D.C.) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA-TM (National Advisory Committee for Aeronautics, 1920) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA-TN (NACA, 1920) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA transonic wind-tunnel test sections (U.S. Government Printing Office, 1955), also by Ray H. Wright and Vernon G. Ward (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA-University conference on aerodynamics, construction, and propulsion [held at] Lewis Flight Propulsion Laboratory, Cleveland, Ohio, October 20, 21, and 22, 1954. ([Washington?], 1954) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: NACA-University conference on aerodynamics, construction, propulsion : [held at] Lewis Flight Propulsion Laboratory, Cleveland, Ohio, October 20, 21, and 22, 1954. (s.n., 1954) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The N.A.C.A. variable-density wind tunnel (Government Printing Office, 1932), also by Eastman N. Jacobs and Ira H. Abbott (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: NACA VGH recorder (National Advisory Committee for Aeronautics, 1951), also by Norman R. Richardson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Robert S. Swanson, E. LaVerne Priddy, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert T. Jones and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Neal Tetervin and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by John A. Zalovcik, Clotaire Wood, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Jack Fischel and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Carl F. Schueller, H. Kurt Strass, Peter F. Korycinski, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Charles L. Seacord, Herman O. Ankenbruck, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Marion O. McKinney and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryansky, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Paul Kuhn, Simon H. Diskin, John E. Duberg, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Robert Gottlieb and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Mason F. Miller and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Robert Gottlieb and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Eugene E. Lundquist, W. D. Kroll, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Joseph N. Kotanchik, Robert A. Weinberger, Walter Woods, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Charles M. Zimmey, Viola M. Lappi, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Norman Rafel and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert T. Jones, Harry Greenberg, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by George J. Heimerl, J. Albert Roy, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by S. B. Batdorf, John C. Houbolt, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by I. Elizabeth Garner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by H. S. Ribner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Merven W. Mandel, Leonard M. Bartone, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harry E. Murray, Mary A. Erwin, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by J. D. Bird and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by H. S. Ribner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold F. Kleckner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Hubert M. Drake and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold I. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by W. H. Gray and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John A. Zalovcik, Fred L. Daum, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Norris F. Dow, William A. Hickman, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by S. B. Batdorf, Charles Libove, Manuel Stein, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John A. Zalovcik and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Donald D. Baals, Norman F. Smith, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Antonio Ferri and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by I. E. Garrick, Carl Kaplan, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Irven Naiman and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John L. Crigler and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by A. I. Neihouse and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Clifford S. Gardner, James A. LaHatte, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Blake W. Corson, Mason F. Miller, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Carl Kaplan and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Walter A. Bartlett and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by E. O. Pearson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert B. Liddell and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by F. B. Gustafson, William J. O'Sullivan, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Sidney A. Batterson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Marvin Pitkin and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Charles W. Mathews, Clotaire Wood, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Walter C. Williams and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Harry Greenberg and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Paul A. Hunter, John P. Reeder, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Irven Naiman and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by H. S. Ribner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by I. E. Garrick, Carl Kaplan, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Thomas A. Hollingworth and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by S. M. Harmon and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold I. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Paul E. Purser, Elizabeth G. McKinney, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Marvin Pitkin, Robert O. Schade, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Harold I. Johnson, Joseph R. Vensel, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by William H. Phillips and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert B. Liddell, Vernard E. Lockwood, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by William Mutterperl and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Aircraft Engine Research Laboratory, 1944), also by Rinaldo J. Brun, Cearcy D. Miller, H. Lowell Olsen, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Robert W. Kamm, Frank S. Malvestuto, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold F. Kleckner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Robert S. Swanson, Stewart M. Crandall, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John P. Campbell, John W. Paulson, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Gerald G. Kayten, William Koven, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Jack Fischel, John M. Riebe, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Thomas A. Hollingworth and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by E. O. Pearson, F. E. West, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Carl A. Sandahl and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Leo F. Fehlner, Robert MacLachlan, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Jack Norman Nielsen, Harold H. Sweberg, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Upshur T. Joyner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by F. B. Gustafson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Myron J. Block, S. Katzoff, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John L. Crigler, Herbert W. Talkin, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Oscar Seidman and Langley Air Force Base (Va.). Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by W. H. Phillips, P. A. Hunter, H. L. Crane, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by William H. Phillips and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John P. Campbell, Charles L. Seacord, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Ray H. Wright and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by De E. Beeler and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by John A. Zalovcik, Fred L. Daum, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Arthur Kantrowitz and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by J. D. Bird and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Chester H. Wolowicz and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Clotaire Wood, John A. Zalovcik, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by M. Leroy Spearman and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Thomas A. Toll, Margaret F. Ivey, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by William H. Phillips and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Ralph P. Bielat and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by W. F. Lindsey and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Milton D. Humphreys and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Jerold M. Bidwell, David M. Goldenbaum, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Sidney A. Batterson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Sidney A. Batterson, Thelma Stewart, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Wilbur L. Mayo and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by W. F. Lindsey and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Harry E. Murray, Clarence L. Gillis, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Joseph N. Kotanchik, George W. Zender, Walter Woods, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Douglas A. King, Newton A. Mas, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John M. Riebe, Elizabeth G. McKinney, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Carl F. Schueller, Peter F. Korycinski, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Leo F. Fehlner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Marvin Pitkin, Charles V. Bennett, John W. Draper, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Blake W. Corson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Jerry Goodman and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Cloyce E. Matheny and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by J. Ford Johnston, T. J. Voglewede, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Evan H. Schuette and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Walter C. Williams and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Robert Gottlieb, Merven W. Mandel, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1940), also by Eugene E. Lundquist, Joseph N. Kotanchik, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Theodore Theodorsen, Arthur A. Regier, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1941), also by Abe Silverstein, Eugene R. Guryansky, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by W. C. Williams and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Sidney A. Batterson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Marvin Schuldenfrei and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by H. Page Hoggard, Marjorie E. Bulloch, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1941), also by J. M. Nissen, M. D. White, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Eugene E. Lundquist and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Evan H. Schuette, J. Albert Roy, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by S. Katzoff, Robert S. Finn, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by John P. Campbell, Thomas A. Hollingworth, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Robert T. Jones, Joseph W. Wetmore, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Doris Cohen and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen, Arthur A. Regier, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert S. Swanson, Stewart M. Crandall, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by George J. Heimerl, J. Albert Roy, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John M. Riebe, Oleta Church, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by A. W. Vogeley and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by H. A. Pearson, William S. Aiken, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert R. Gilruth and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Richard T. Whitcomb and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Marion O. McKinney, Bernard Maggin, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by F. B. Gustafson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Richard V. Rhode, Philip Donely, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Robert H. Neely, D. William Conner, Richard W. Fairbanks, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Warren A. Tucker, Arthur R. Wallace, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John H. Quinn, Warren A. Tucker, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John A. Zalovcik, Richard B. Skoog, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John A. Zalovcik and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Laurence K. Loftin and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by William J. Underwood, Jones F. Cahill, Albert L. Braslow, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Albert L. Braslow and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Felicien F. Fullmer and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (NACA, in the 1940s), also by Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (NACA, in the 1940s), also by Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Albert E. Von Doenhoff, Louis S. Stivers, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Norman S. Land and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Frank T. Abbott and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Donald D. Baals, Mary J. Mourhess, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1943), also by Alun R. Jones, Lewis A. Rodert, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1945), also by Carr Neel and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1941), also by Lewis A. Rodert, Lawrence A. Clousing, William H. McAvoy, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1944), also by Robert M. Crane, Ralph W. Holtzclaw, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1944), also by Robert M. Crane, Ralph W. Holtzclaw, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1943), also by Jerome L. Kushnick and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1945), also by Thomas L. Keller, Robert F. Keuper, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1942), also by William H. McAvoy, Lawrence A. Clousing, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1944), also by Harry J. Goett, Noel K. Delany, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1945), also by William N. Turner, Lawrence A. Clousing, Paul J. Steffen, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1944), also by John T. Sinnette, J. Austin King, Oscar W. Schey, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by William K. Ritter, Irving A. Johnsen, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by J. Austin King, Harold Klein, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1944), also by J. Austin King, Owen W. Regan, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1942), also by Herman H. Ellerbrock, Arthur W. Goldstein, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by William A. Benser, Jason J. Moses, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by William K. Ritter, William L. Beede, Ambrose Ginsburg, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by W. Perl, M. Tucker, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by Benjamin Pinkel, Everett Bernardo, Eugene J. Manganiello, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by W. E. Moeckel, J. C. Evvard, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), also by R. C. Spencer, A. W. Jones, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), also by Arnold E. Biermann, Lester C. Corrington, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), also by Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by Everett Bernardo, Carroll S. Eian, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), also by Harvey A. Cook, W. T. Olson, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1944), also by John H. Collins, Ralph F. Schmiedlin, E. E. Bisson, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1944), also by Charles S. Moore, Fred Voss, Arnold E. Biermann, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), also by J. C. Sanders, B. A. Mulcahy, H. D. Wilsted, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by Carl L. Meyer, J. Robert Branstetter, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by Ernest R. Chanes, L. Robert Carman, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by David S. Gabriel, L. Robert Carman, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), also by J. C. Sanders, Alexander Mendelson, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Anthony W. Jones, Edmund R. Jonash, Arthur W. Bull, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Edmund R. Jonash, J. Robert Branstetter, Carl L. Meyer, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Carl L. Meyer, J. Robert Branstetter, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Cearcy D. Miller, J. Robert Branstetter, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Cearcy D. Miller and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Henry E. Alquist, John C. Evvard, Leon O'Dell, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Earl E. Coulter, David S. Gabriel, Robert G. Larkin, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Donald G. Guentert, John G. Ferkan, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Michael F. Valerino, Richard F. Hughes, Robert H. Essig, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Gilbert E. Chapman and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), also by Edmund J. Baas, Paul D. Dugan, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Richard C. Dingeldein, Raymond F. Schaefer, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Harold I. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1946), also by Hubert M. Drake and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by James P. Peterson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by J. D. Bird and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by James P. Peterson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Myron J. Block, S. Katzoff, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Roy H. Lange and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryanksy, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by F. J. Bailey, F. B. Gustafson, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by H. Page Hoggard and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by Paul Kuhn, L. Ross Levin, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Francis M. Rogallo, Paul E. Purser, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Harold E. Cleary and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by Harold E. Cleary and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by John G. Lowry, I. Elizabeth Garner, James A. Maloney, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Robert E. Pendley and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by James M. Benson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by Merven W. Mandel, Evan H. Schuette, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Isidore G. Recant, Arthur R. Wallace, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by William J. Underwood, Frank T. Abbott, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by John W. McKee, Robert B. Liddell, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), also by Ira H. Abbott and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Ira H. Abbott and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by George P. Wood, D. E. Brimley, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), also by John G. Lowry and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), also by John G. Lowry and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by John G. Lowry, Thomas A. Toll, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Isidore G. Recant, Robert S. Swanson, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Natural icing of an axial-flow turboject engine in flight for a single icing condition (National Advisory Committee for Aeronautics, 1948), also by Loren W. Acker and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The near noise field of static jets and some model studies of devices for noise reduction (National Advisory Committee for Aeronautics, 1954), also by Leslie W. Lassiter and Harvey H. Hubbard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The near noise field of static jets and some model studies of devices for noise reduction (U.S. Government Printing Office, 1956), also by Leslie W. Lassiter and Harvey H. Hubbard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Neustoichivye kapilliarnye volny na poverkhnosti razdela dvukh vyazkikh zhidkostei (National Advisory Committee for Aeronautics, 1951), also by V. A. Borodin and Y. F. Dityakin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A new simple interferometer for obtaining quantitatively evaluable flow patterns (NACA, 1953), also by S. F. Erdmann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Nomenclature for aeronautics (For sale by the Superintendent of Document, 1933) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Nomenclature for aeronautics ([U.S. Govt. Print. Off.], 1941) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Nomenclature for aeronautics. (Govt. Print. Off., 1920) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Nonlinear theory of a hot-wire anemometer (NACA, 1952), also by R. Betchov (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Nonmetallic material compatibility with liquid fluorine (National Advisory Committee for Aeronautics, 1957), also by Harold G. Price and Howard W. Douglass (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Nonstationary gas flow in thin pipes of variable cross section (NACA, 1948), also by G. Guderley and Dave Feingold (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Normal component of induced velocity in the vicinity of a lifting rotor with a nonuniform disk loading (National Advisory Committee for Aeronautics, 1956), also by Harry H. Heyson and S. Katzoff (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application (National Advisory Committee for Aeronautics, 1953), also by Walter Castles and Jacob Henri De Leeuw (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05 (National Advisory Committee for Aeronautics, 1954), also by Edward F. Ulmann, Robert W. Dunning, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Note of similarity conditions for flows with heat transfer (National Advisory Committee for Aeronautics, 1948), also by Albert E. Von Doenhoff (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Note on hovering turns with tandem helicopters (National Advisory Committee for Aeronautics, 1955), also by John P. Reeder and Robert J. Tapscott (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Note on performance of aircraft ejector nozzles at high secondary flows (National Advisory Committee for Aeronautics, 1954), also by Fred D. Kochendorfer and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A note on secondary flow in rotating radial channels (National Advisory Committee for Aeronautics, 1953), also by James J. Kramer and John D. Stanitz (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack (National Advisory Committee for Aeronautics, 1949), also by Laurence K. Loftin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Note on the calculation of boundary layers (National Advisory Commitee for Aeronautics, 1940), also by Ludwig Prandtl (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Note on the importance of imperfect-gas effects and variation of heat capacities on the isentropic flow of gases (NACA, 1948), also by Coleman duP. Donaldson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Notes on the technique of landing airplanes equipped with wing flaps (National Advisory Committee for Aeronautics, 1936), also by Melvin N. Gough (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Numerical approach to the instability problem of monocoque cylinders (National Advisory Committee for Aeronautics, 1951), also by Bruno A. Boley, Mayers. J., and Josesph Kempner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions (National Advisory Committee for Aeronautics, 1950), also by Richard R. Heldenfels (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Oberflachenrauhigkeiten auf Tragflugeln. (National Advisory Committee for Aeronautics ;, 1926), also by O. Schrenk (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On a class of exact solutions of the equations of motion of a viscous fluid (NACA, 1953), also by V. I. Yatseyev (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On a solution of the nonlinear differential equation for transonic flow past a wave-shaped wall (National Advisory Committee for Aeronautics, 1951), also by Carl Kaplan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On a source-sink method for the solution of the Prandtl-Busemann iteration equations in two-dimensional compressible flow (National Advisory Committee for Aeronautics, 1950), also by Keith C. Harder and E. B. Klunker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On combustion in a turbulent flow (NACA, 1947), also by K. I. Shelkin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On motion of fluid in boundary layer near line of intersection of two planes (NACA, 1951), also by L. G. Loĭt�si�anskiĭ and V. P. Bolshakov (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On rotational conical flow (NACA, 1952), also by Carlo Ferrari (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On slender-body theory at transonic speeds (NACA, 1954), also by Keith C. Harder, E. B. Klunker, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On stability and turbulence of fluid flows (NACA, 1951), also by Werner Heisenberg (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the application of the energy method to stability problems (NACA, 1947), also by K. Marguerre (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the contribution of turbulent boundary layers to the noise inside a fuselage (NACA, 1956), also by G. M. Corcos and H. W. Liepmann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the design of airfoils in which the transition of the boundary layer is delayed (NACA, 1952), also by Itiro Tani (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the determination of certain basic types of supersonic flow fields (NACA, 1954), also by Carlo Ferrari (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the gas dynamics of a rotating impeller (NACA, 1956), also by Adolf Busemann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the instability of methods for the integration of ordinary differential equations (NACA, 1956), also by Heinz Rutishauser (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow (National Advisory Committee for Aeronautics, 1954), also by Charles E. Watkins, Donald S. Woolston, and Harry L. Runyan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the problem of gas flow over an infinite cascade using Chaplygin's approximation (NACA, 1951), also by G. A. Bugaenko (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the range of applicability of the transonic area rule (NACA, 1954), also by John R. Spreiter and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the recording of turbulent longitudinal and transverse fluctuations (NACA, 1951), also by Helmut Reichardt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the representation of the stability region in oscillation problems with the aid of the Hurwitz determinants (NACA, 1952), also by E. Sponder (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the Second-order tunnel-wall-constriction corrections in two-dimensional compressible flow (National Advisory Committee for Aeronautics, 1951), also by E. B. Klunker and Keith C. Harder (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the spectrum of natural oscillations of two-dimensional laminar flows (NACA, 1957), also by D. Grohne (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the stability of the free laminar boundary layer between parallel streams (National Advisory Committee for Aeronautics, 1949), also by Martin Lessen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the statistical theory of turbulence (National Advisory Committee for Aeronautics, 1958), also by Werner Heisenberg (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the theory of oscillating airfoils of finite span in subsonic compressible flow (National Advisory Committee for Aeronautics, 1949), also by Eric Reissner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the theory of the Laval nozzle (NACA, 1949), also by S. V. Falkovich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the theory of the turbulent boundary layer (National Advisory Committee for Aeronautics, 1953), also by Julius C. Rotta (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the three-dimensional instability of laminar boundary layers on concave walls (NACA, 1954), also by Henry Görtler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the turbulent friction layer for rising pressure (NACA, 1951), also by K. Wieghardt and W. Tillmann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On the use of the harmonic linearization method in the automatic control theory (NACA, 1957), also by E. P. Popov (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On transonic flow past a wave-shaped wall (National Advisory Committee for Aeronautics, 1952), also by Carl Kaplan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: On two-dimensional supersonic flows (National Advisory Committee for Aeronautics ;, 1949), also by Stefan Bergman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: One-dimensional analysis of choked-flow turbines (National Advisory Committee for Aeronautics, 1952), also by Robert E. English and Richard H. Cavicchi (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: One-dimensional flow of an imperfect diatomic gas (National Advisory Committee for Aeronautics, 1949), also by A. J. Eggers (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Operational characteristics (National Advisory Committee for Aeronautics, 1948), also by Richard L. Golladay, Stanley L. Gendler, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Operational characteristics (National Advisory Committee for Aeronautics, 1948), also by William A. Fleming and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The organization, research activities and facilities of the NACA. ([Washington], 1948) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Oscillating pressures near a static pusher propeller at tip Mach numbers up to 1.20 with special reference to the effects of the presence of the wing (National Advisory Committee for Aeronautics, 1954), also by Harvey H. Hubbard and Leslie W. Lassiter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Over-all engine performance (National Advisory Committee for Aeronautics, 1948), also by J. C. Nettles, J. R. Easterly, and Flight Propulsion Research Laboratory (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Oxidation of titanium carbide base ceramals containing molybdenum, tungsten, and cobalt (National Advisory Committee for Aeronautics, 1949), also by M. J. Whitman and A. J. Repko (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Perforated supersonic inlet (National Advisory Committee for Aeronautics, 1948), also by Albert H. Schroeder, James F. Connors, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), also by William A. Fleming, Robert O. Jr Dietz, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), also by William A. Fleming and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance characteristics of plane-wall two-dimensional diffusers (National Advisory Committee for Aeronautics, 1953), also by Elliott G. Reid (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine (National Advisory Committee for Aeronautics, 1950), also by William P. Cook, Richard G. Koch, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance of a translating-double-cone axisymmetric inlet with cowl bypass at mach number from 2.0 to 3.5 (National Advisory Committee for Aeronautics, 1957), also by James F. Connors, GeorgeA. Wise, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance of basic XJ79-GE-1 turbojet engine and its components. (National Advisory Committee for Aeronautics, 1961), also by Carl E. Campbell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance of basic XJ79-GE-1 turbojet engine and its components (National Advisory Committee for Aeronautics, 1958), also by Carl E. Campbell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight. [Part] I, U-shaped channel walls for secondary-air entry / (National Advisory Committee for Aeronautics, 1955), also by Eugene V. Zettle, Robert Friedman, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Performance of J33 turbojet engine with shaft-power extraction [Part] 2, Compressor (National Advisory Committee for Aeronautics, 1948), also by Albert O. Ross, J. Cary Nettles, J. R. Easterly, and Flight Propulsion Research Laboratory (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Performance of supersonic axial-flow compressors based on one-dimensional analysis (National Advisory Committee for Aeronautics, 1949), also by Linwood C. Wright, John F. Klapproth, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Photographic investigation of air-flow patterns in transparent one-sixth sector of annular turbojet-engine combustor with axial-slot-type air admission (National Advisory Committee for Aeronautics, 1954), also by Charles C. Graves, J. Dean Gernon, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Photographic studies of preignition environment and flame initiation in turbojet-engine combustors (National Advisory Committee for Aeronautics, 1953), also by David M. Straight, J. Dean Gernon, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The physical properties of active nitrogen in low-density flow (National Advisory Committee for Aeronautics, 1951), also by James M. Benson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The plane problem of the flapping wing (NACA, 1954), also by Walter Birnbaum (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preignition-limited performance of several fuels (U.S. Government Printing Office, 1945), also by Donald W. Male and John C. Evvard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary attempts at isothermal compression of a supersonic air stream (National Advisory Committee for Aeronautics, 1956), also by E. Perchonok, F. Wilcox, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A preliminary determination of normal accelerations on racing airplanes (National Advisory Committee for Aeronautics, 1935), also by Nathan F. Scudder and H. W. Kirschbaum (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary engine investigation (National Advisory Committee for Aeronautics, 1949), also by Andre J. Meyer, Howard F. Calvert, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation at supersonic speeds of triangular and sweptback wings (National Advisory Committee for Aeronautics, 1949), also by Macon C. Ellis and Lowell E. Hasel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios (National Advisory Committee for Aeronautics, 1953), also by Eli Reshotko and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of a variable Mach number two-dimensional supersonic tunnel of fixed geometry (National Advisory Committee for Aeronautics, 1949), also by William J. Nelson, Frederick Bloetscher, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of needle bearings of 1 1/8-inch pitch diameter at speeds to 17,000 rpm (National Advisory Committee for Aeronautics, 1949), also by E. Fred Macks (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of supersonic diffusers (Langley Memorial Aeronautical Laboratory, 1945), also by Arthur Kantrowitz, Coleman duP. Donaldson, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of the characteristics of a two-dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane (National Advisory Committee for Aeronautics, 1957), also by David H. Hickey and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of the compressive strength and creep lifetime of 2024-T3 (formerly 24S-T3) aluminum-alloy plates at elevated temperatures (National Advisory Committee for Aeronautics, 1955), also by Eldon E. Mathauser, William D. Deveikis, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of the failure of pressurized stiffened cylinders (National Advisory Committee for Aeronautics, 1955), also by Norris F. Dow, Roger W. Peters, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of the strength and endurance of plastic-impregnated fiberglass compressor blades (National Advisory Committee for Aeronautics, 1955), also by Donald F. Johnson, Andre J. Meyer, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of the use of afterglow for visualizing low-density compressible flows (National Advisory Committee for Aeronautics, 1949), also by Thomas W. Williams and James M. Benson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary investigation of wear and friction. Properties under sliding conditions of materials suitable for cages of rolling-contact bearings (National Advisory Committee for Aeronautics, 1951), also by Robert L. Johnson, E. E. Bisson, and Max A. Swikert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary measurements of atmospheric turbulence at high altitude as determined from acceleration measurements on Lockheed U-2 airplane (National Advisory Committee for Aeronautics, 1957), also by Thomas L. Coleman and Jack Funk (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary metallographic studies of ball fatigue under rolling-contact conditions (National Advisory Committee for Aeronautics, 1957), also by H. Robert Bear and Robert H. Butler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary report on a study of separated flows in supersonic and subsonic streams (National Advisory Committee for Aeronautics, 1956), also by Dean R. Chapman, Howard K. Larson, Donald M. Kuehn, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary studies of rolling-contact fatigue life of high-temperature bearing materials (National Advisory Committee for Aeronautics, 1958), also by Thomas L. Carter, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary study of applied load factors in bumpy air (National Advisory Committee for Aeronautics ;, 1931), also by Richard V. Rhode and Eugene E. Lundquist (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary survey of possible cooling methods for hypersonic aircraft (NACA, 1958), also by Jack B. Esgar, Francis S. Stepka, Robert O. Hickel, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics (U.S. G.P.O., 1925), also by Max M. Munk (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Preparation and properties of concentrated boron-hydrocarbon slurry fuels (National Advisory Committee for Aeronautics, 1954), also by Irving A. Goodman, Virginia O. Fenn, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 (NACA, 1952), also by Leo T. Chauvin and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Pressure distribution and some effects of viscosity on slender inclined bodies of revolution (National Advisory Committee for Aeronautics, 1950), also by H. Julian Allen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Pressure distribution over a semicircular wing tip on a biplane in flight (National Advisory Committee for Aeronautics ;, 1931), also by Richard V. Rhode and Eugene E. Lundquist (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Pressure distributions on three bodies of revolution to determine the effect of Reynolds number up to and including the transonic speed range (NACA, 1953), also by John M. Swihart and Charles F. Whitcomb (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Pressure-sensitive system for gas-temperature control (National Advisory Committee for Aeronautics, 1948), also by Norman Matz, Richard S. Cesaro, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Primer tochnogo reshenia ploskoi vikhrevoi zadachi gazovoi dinamiki (National Advisory Committee for Aeronautics, 1950), also by I. A. Kiebel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Principal effects of axial load on moment-distribution analysis of rigid structures (National Advisory Committee for Aeronautics, 1935), also by Benjamin Wylie James (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Problem of slip flow in aerodynamics (National Advisory Committee for Aeronautics, 1957), also by Robert E. Street (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The problem of torsion in prismatic members of circular segmental cross section (NACA, 1948), also by A. Weigand (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Procedure for calculating turbine blade temperatures and comparison of calculated with observed values for two stationary air-cooled blades (NACA, 1952), also by W. Byron Brown, Hadley T. Richards, Henry O. Slone, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Profilmessungen im DVL-Hochgeschwindigkeitswindkanal (2,7-meter Durchmesser) (National Advisory Committee for Aeronautics, 1949), also by B. Göthert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Propagation of sound into a wind-created shadow zone (National Advisory Committee for Aeronautics, 1957), also by David C. Pridmore-Brown (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Propeller-noise charts for transport airplanes (National Advisory Committee for Aeronautics, 1953), also by Harvey H. Hubbard (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The proper combination of lift loadings for least drag on a supersonic wing (National Advisory Committee for Aeronautics, 1955), also by Frederick C. Grant (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Properties and preparation of ceramic insulators for spark plugs (G.P.O., 1919) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Properties of honeycomb cores as affected by fiber type, fiber orientation, resin type, and amount (National Advisory Committee for Aeronautics, 1951), also by R. J. Seidl, A. W. Voss, and D. J. Fahey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Qualitative measurements of the effective heats of ablation of several materials in supersonic air jets at stagnation temperatures up to 11,000À F (NACA, 1958), also by Bernard Rashis, Russell N. Hopko, William G. Witte, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Ramp floor vent-tube mounting (National Advisory Committee for Aeronautics, 1948), also by Robert S. Ruggeri and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Reaction of fluorine with carbon as a means of fluorine disposal (National Advisory Committee for Aeronautics, 1957), also by Harold W. Schmidt (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Recent control studies (National Advisory Committee for Aeronautics, 1959), also by John G. Lowry (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Recent data on tire friction during landing (National Advisory Committee for Aeronautics, 1957), also by Sidney A. Batterson (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Reciprocity relations in aerodynamics (National Advisory Committee for Aeronautics, 1952), also by Max A. Heaslet and John R. Spreiter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams (NACA, 1954), also by Frederick S. Simmons and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A recurrence matrix solution for the dynamic response of aircraft in gusts (National Advisory Committee for Aeronautics, 1950), also by John C. Houbolt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Relation of turbine-engine combustion efficiency to second-order reaction kinetics and fundamental flame speed (National Advisory Committee for Aeronautics, 1954), also by J. Howard Childs, Charles C. Graves, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Remark on the theory of lifting surfaces (NACA, 1956), also by Aldo Muggia (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Report (G.P.O., 1915) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Report. (U.S. Govt. Print. Office, 1915) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Research abstracts (National Advisory Committee for Aeronautics, 1951) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Research memorandum. (National Advisory Committee for Aeronautics, in the 20th century) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Research memorandum. Series H. (Washington, D.C.) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Resistance of cascade of airfoils in gas stream at subsonic velocity (NACA, 1951), also by L. G. Loĭt�si�anskiĭ (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range (National Advisory Committee for Aeronautics, 1951), also by WIlliam T. Lauten, Herbert C. Nelson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The reversibility theorem for thin airfoils in subsonic and supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Clinton E. Brown (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A review of analytical methods for the treatment of flows with detached shocks (National Advisory Committee for Aeronautics, 1949), also by Adolf Busemann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Review of emulsified antifoams for aircraft lubricating oils (National Advisory Committee for Aeronautics, 1949), also by W. W. Woods and J. V. Robinson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A review of the physical and thermodynamic properties of boric oxide (NACA, 1957), also by Paul C. Setze and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60° delta wing and a high unwept horizontal tail (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Robert F. Peck, Jesse L. Mitchell, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Role of nickel dip in enameling of sheet steel (National Advisory Committee for Aeronautics, 1954), also by D. G. Moore, W. N. Harrison, and J. W. Pitts (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Rolling and yawing moments for swept-back wings in sideslip at supersonic sppeds (National Advisory Committee for Aeronautics, 1951), also by Seymour Lampert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Edward C. Polhamus, William C. Sleeman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Rotor blades with 34 steel tubes in cooling-air passages (National Advisory Committee for Aeronautics, 1950), also by Robert O. Hickel, Gordon T. Smith, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Rotor blades with split trailing edges (National Advisory Committee for Aeronautics, 1951), also by Gordon T. Smith, Robert O. Hickel, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A semi-graphical method for analyzing strains measured on three or four gage lines intersecting at 45 degrees (National Advisory Committee for Aeronautics, 1939), also by H. N. Hill (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A semiempirical method for estimating the rolling moment due to yawing of airplanes (National Advisory Committee for Aeronautics, 1949), also by John P. Campbell and Alex Goodman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Seven commercial organo-metallic additives (National Advisory Committee for Aeronautics, 1954), also by Vincent F. Hlavin, William P. Cook, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The shearing rigidity of curved panels under compression (National Advisory Committee for Aeronautics, 1946), also by Nicholas J. Hoff and Bruno A. Boley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Similarity laws for transonic flow about wings of finite span (National Advisory Committee for Aeronautics, 1951), also by John R. Spreiter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Simple method of estimating the subsonic lift and damping in roll of sweptback wings (National Advisory Committee for Aeronautics, 1949), also by Edward C. Polhamus (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A simple numerical method for the calculation of the laminar boundary layer (National Advisory Committee for Aeronautics, 1952), also by K. Schröder (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver (National Advisory Committee for Aeronautics, 1956), also by Leonard Sternfield, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Simulated afterburner performance with hydrogen peroxide injection for thrust augmentation (National Advisory Committee for Aeronautics, 1956), also by Allen J. Metzler, Jack S. Grobman, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air (National Advisory Committee for Aeronautics, 1950), also by Eugene V. Zettle, Herman Mark, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Simulator studies of jet reaction controls for use at high altitude (National Advisory Committee for Aeronautics, 1958), also by Wendell H. Stillwell, Hubert M. Drake, and Flight Research Center (U.S.) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment (National Advisory Committee for Aeronautics, 1951), also by Harry L. Runyan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Small bending and stretching of sandwich-type shells (National Advisory Committee for Aeronautics, 1949), also by Eric Reissner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Solutions for hydrodynamic impact force and response of a two-mass system with an application to an elastic airframe (National Advisory Committee for Aeronautics, 1947), also by Wilbur L. Mayo (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some approximate equations for the standard atmosphere (Government Printing Office, 1931), also by Walter S. Diehl (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3 (National Advisory Committee for Aeronautics, 1959), also by M. Leroy Spearman and Arthur Henderson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some effects of blade trailing-edge thickness on performance of a single-stage axial-flow compressor (National Advisory Committee for Aeronautics, 1951), also by J. J. Moses, G. K. Serovy, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some effects of density and Mach number on the flutter speed of two uniform wings (National Advisory Committee for Aeronautics, 1949), also by George E. Castile and Robert W. Herr (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing (National Advisory Committee for Aeronautics, 1954), also by Roland D. English, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some effects of fluid in pylon-mounted tanks on flutter (National Advisory Committee for Aeronautics, 1955), also by James R. Reese (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw (National Advisory Committee for Aeronautics, 1952), also by John D. Bird, Sadie M. Hubbard, and Lewis R. Fisher (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310À and 3,500À R on a magnesium fin with several leading-edge modifications (NACA, 1957), also by W. M. Bland, Walter E. Bressette, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some elementary principles of shell stress analysis with notes on the use of the shear center (National Advisory Committee for Aeronautics, 1939), also by Paul Kuhn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag (NACA, 1957), also by Robert L. Nelson, Clement J. Welsh, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some experiences regarding the nonlinearity of hot wires (NACA, 1952), also by Robert Betchov and W. Welling (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some factors affecting the variation of pitching moment with sideslip of aircraft configurations (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Edward C. Polhamus and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some investigations of the general instability of stiffened metal cylinders. 9 - Criterions for the design of stiffened metal cylinders subject to general instability failures (National Advisory Committee for Aeronautics ;, 1947), also by Louis G. Dunn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some measurements of boiling burn-out (National Advisory Committee for Aeronautics, 1955), also by Warren H. Lowdermilk and Walter F. Weiland (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some measurements of time and space correlation in wind tunnel (NACA, 1955), also by Alexandre Favre, R. Dumas, and J. Gaviglio (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some methods of analyzing the effect of basic design variables on axial-flow-compressor performance (National Advisory Committee for Aeronautics, 1947), also by John T. Sinnette and Flight Propulsion Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some notes on the aerodynamic loads associated with external-store installations (National Advisory Committee for Aeronautics, 1953), also by H. Norman Silvers, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some observations on loss of static strength due to fatigue cracks (National Advisory Committee for Aeronautics, 1955), also by Walter Illg, Herbert F. Hardrath, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some possibilities of using gas mixtures other than air in aerodynamic research (National Advisory Committee for Aeronautics, 1954), also by Dean R. Chapman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some properties of high-purity sintered wrought molybdenum metal at temperatures up to 2400° F (National Advisory Committee for Aeronautics, 1951), also by R. A. Long, H. R. Bear, and K. C. Dike (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some recent research on the handling qualities of airplanes (National Advisory Committee for Aeronautics, 1956), also by Walter C. Williams, William H. Phillips, Flight Research Center (U.S.), and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some theoretical characteristics of trapezoidal wings in supersonic flow and a comparison of several wing-flap combinations (National Advisory Committee for Aeronautics, 1951), also by Robert O. Piland (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip (National Advisory Committee for Aeronautics, 1949), also by John D. Bird (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Span loadings due to wing twist at transonic and supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by Frederick C. Grant, John P. Mugler, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A special investigation to develop a general method for thee-dimensional photoelastic stress analysis (National Advisory Committee for Aeronautics, 1952), also by Max Mark Frocht and R. Guernsey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Spectrum of turbulence in a contracting stream (National Advisory Committee for Aeronautics, 1952), also by Herbert Spencer Ribner and Maurice Tucker (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Spin tests of two models of a low-wing monoplane to investigate scale effect in the model test range (National Advisory Committee for Aeronautics, 1941), also by Charles J. Donlan (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes (National Advisory Committee for Aeronautics, 1951), also by Walter J. Klinar and Jack H. Wilson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery (National Advisory Committee for Aeronautics, 1949), also by Anshal I. Neihouse and M. S. Uberoi (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Spinning and related problems at high angles of attack for high-speed airplanes (National Advisory Committee for Aeronautics, 1956), also by Walter J. Klinar, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Spiral motions of viscous fluids (NACA, 1953), also by Georg Hamel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stability derivatives of triangular wings at supersonic speeds (National Advisory Committee for Aeronautics, 1948), also by H. S. Ribner and Frank S. Malvestuto (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stability of systems containing a heat source - the Rayleigh criterion (National Advisory Committee for Aeronautics, 1956), also by Boa-Teh Chu (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4 (National Advisory Committee for Aeronautics, 1957), also by Reginald R. Lundstrom, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stalling of helicopter blades (National Advisory Committee for Aeronautics ;, 1946), also by F. B. Gustafson and G. C. Myers (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Standard aeronautical symbols ([Washington, D.C.?] : National Advisory Committee for Aeronautics, 1940., 1940) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Standard nomenclature for airspeeds with tables and charts for use in calculation of airspeed (National Advisory Committee for Aeronautics ;, 1946), also by William J. Aiken (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid (National Advisory Committee for Aeronautics, 1950), also by Gerald Morrell, Jack C. Humphrey, John L. Sloop, Dezso J. Ladanyi, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Static investigation of several jet deflectors for longitudinal control of an aircraft (National Advisory Committee for Aeronautics, 1955), also by Alfred S. Valerino and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The static longitudinal characteristics of a twisted and cambered 45⁰ sweptback wing at mach numbers up to 0.96 (National Advisory Committee for Aeronautics, 1958), also by Robert I. Sammonds and Robert M. Reynolds (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine (National Advisory Committee for Aeronautics, 1955), also by Reeves P. Cochran, Robert P. Dengler, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Static shear strength of 2117-T4 (A17s-T4) aluminum-alloy rivets at elevated temperatures (National Advisory Committee for Aeronautics, 1956), also by W. J. Dewalt and K. O. Bogardus (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Statistical measurements of contact conditions of 478 transport-airplane landings during routine daytime operations (National Advisory Committee for Aeronautics, 1954), also by Norman S. Silsby (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Statistical survey of icing data measured on scheduled airline flights over the United States and Canada from November 1951 to June 1952 (National Advisory Committee for Aeronautics, 1955), also by Porter J. Perkins (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds (National Advisory Committee for Aeronautics, 1957), also by John M. Swihart and Norman L. Crabill (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Strain-gage study of internally cooled exhaust valves having various throat designs (National Advisory Committee for Aeronautics ;, 1946), also by Arthur G. Holms and Richard D. Faldetta (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Strength of heat-resistant laminates up to 375° C (National Advisory Committee for Aeronautics, 1951), also by B. M. Axilrod and Martha A. Sherman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Strength tests on paper cylinders in compression, bending, and shear (National Advisory Committee for Aeronautics ;, 1931), also by Richard V. Rhode and Eugene E. Lundquist (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stress analysis of beams with shear deformation of the flanges. ([Washington] : [U.S. G.P.O.], 1937., 1937), also by Paul Kuhn (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Stress analysis of circular semimonocoque cylinders with cutouts by a perturbation load technique (National Advisory Committee for Aeronautics, 1954), also by Harvey G. McComb (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stress distributions caused by three types of loading on a circular semimonocoque cylinder with flexible wings (National Advisory Committee for Aeronautics, 1954), also by Harvey G. McComb (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stress-life relation of the rolling-contact fatigue spin rig (National Advisory Committee for Aeronautics, 1957), also by Robert H. Butler and Thomas L. Carter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Stresses in and general instability of monocoque cylinders with cutouts. VII - Experimental investigation of cylinders having either long bottom cutouts or series of side cutouts. (National Advisory Committee for Aeronautics, 1949), also by Nicholas J. Hoff, Joseph J. Mele, and Bruno A. Boley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A structural-efficiency evaluation of titanium at normal and elevated temperatures (National Advisory Committee for Aeronautics, 1951), also by George J. Heimerl and Paul F. Barrett (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Structural response to discrete and continuous gusts of an airplane having wing-bending flexibility and a correlation of calculated and flight results (U.S. Government Printing Office, 1954), also by John C. Houbolt and Eldon E. Kordes (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Studies of the lateral-directional flying qualities of a tandem helicopter in forward flight (National Advisory Committee for Aeronautics, 1953), also by Kenneth B. Amer and Robert J. Tapscott (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of effects of heat treatment and hot-cold-work on properties of low-carbon N-155 alloy (National Advisory Committee for Aeronautics, 1949), also by J. W. Freeman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of hypersonic small-disturbance theory (National Advisory Committee for Aeronautics, 1954), also by Milton Van Dyke (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Study of inadvertent speed increases in transport operation (National Advisory Committee for Aeronautics, 1952), also by H. A. Pearson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of liquid boric oxide particle growth rates in a gas stream from a simulated jet engine combustor (National Advisory Committee for Aeronautics, 1957), also by Paul C. Setze, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of means for rationalizing airplane design loads (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by John P. Mayer, Harold A. Hamer, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Study of secondary-flow patterns in an annular cascade of turbine nozzle blades with vortex design (National Advisory Committee for Aeronautics, 1953), also by Harold E. Rohlik, Howard Z. Herzig, and Hubert W. Allen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of the factors affecting the range of airplanes (National Advisory Committee for Aeronautics, 1937), also by David Beirmann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of the flow over a 45À sweptback wing -fuselage combination at transonic Mach numbers (NACA, 1952), also by Richard T. Whitcomb, Thomas C. Kelly, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers (National Advisory Committee for Aeronautics, 1952), also by Coleman duP. Donaldson and Roy H. Lange (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of the response of panels to random acoustic excitation (National Advisory Committee for Aeronautics, 1955), also by R. W. Hess, Harvey H. Hubbard, Leslie W. Lassiter, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results (National Advisory Committee for Aeronautics, 1950), also by John D. Bird and Byron M. Jaquet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Study of unsteady flow disturbances of large and small amplitudes moving through supersonic or subsonic steady flows (National Advisory Committee for Aeronautics, 1949), also by Robert V. Hess and T. Himka (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Study of unsymmetrical-loading conditions (Washington D.C. : National Advisory Committee for Aeronautics 1940., 1940), also by Henry A. Pearson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A study of wing flutter (Washington, D.C. : G.P.O., 1928., 1928), also by A. F. Zahm, Ernest E. Wilson, and United States. Navy. Bureau of Construction and Repair. Aerodynamical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Subject headings for index of NACA publications. (Washington, 1947) (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45° sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶ (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Gene J. Bingham, Albert L. Braslow, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall (National Advisory Committee for Aeronautics, 1949), also by Bernard N. Daley and Lillian E. Hanna (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Suggested method for measuring turbulence (National Advisory Committee for Aeronautics ;, 1931), also by Charles Fayette Taylor (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A summary of available knowledge concerning skin friction and heat transfer and its application to the design of high-speed missiles (NACA, 1951), also by Morris W. Rubesin, Steven A. Varga, Charles B. Rumsey, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A Summary of design formulas for beams having thin webs in diagonal tension (National Advisory Committee for Aeronautics, 1933), also by Paul Kuhn (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A summary of design information for water-cooled turbines (National Advisory Committee for Aeronautics, 1951), also by John C. Freche and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A summary of information on support interference at transonic and supersonic speeds (NACA, 1954), also by Eugene S. Love and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957 (National Advisory Committee for Aeronautics, 1958), also by Martin R. Copp, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A summary of preliminary investigations into the characteristics of combustion screech on ducted burners (National Advisory Committee for Aeronautics, 1954), also by Lewis Laboratory Staff and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Summary of recent theoretical and experimental work on box-beam vibrations (National Advisory Committee for Aeronautics, 1955), also by John M. Hedgepeth, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Summary of results of a wind-tunnel investigation of 9 related horiztonal tails. (National Advisory Committee for Aeronautics, 1955), also by Jules B. Jr Dods, Bruce E. Tinling, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Supersaturation in the spontaneous formation of nuclei in water vapor (NACA, 1953), also by Adolf Sander and Gerhard Damköhler (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model (National Advisory Committee for Aeronautics, 1954), also by William T. Lauten, Joseph H. Judd, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Supersonic lift and pitching moment of thin sweptback tapered wings produced by constant vertical acceleration. Subsonic leading edges and supersonic trailing edges (National Advisory Committee for Aeronautics, 1951), also by Frank S. Malvestuto and Dorothy M. Hoover (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Supplementary note on modified-impact-theory calculations for bodies of revolution having minimum drag at hypersonic speeds (National Advisory Committee for Aeronautics, 1952), also by Meyer M. Resnikoff and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Surface properties of oils (National Advisory Committee for Aeronautics, 1949), also by J. W. McBain and James V. Robinson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Survey of advantages and problems associated with transpiration cooling and film cooling of gas-turbine blades (NACA, 1951), also by E. R. G. Eckert, Jack B. Esgar, and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Survey of hydrogen combustion properties (National Advisory Committee for Aeronautics, 1957), also by Isadore L. Drell, Frank E. Belles, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Survey of hydrogen combustion properties (U.S. Government Printing Office, 1958), also by Isadore L. Drell and Frank E. Belles (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A survey of methods for turbojet thrust measurement applicable to flight installation (National Advisory Committee for Aeronautics, 1955), also by William A. Fleming, David S. Gabriel, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Survey of microstructures and mechanical properties of over-temperatured S-816 turbine buckets from J47 engines (National Advisory Committee for Aeronautics, 1957), also by N. Floreen and R. A. Signorelli (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Survey of portions of the chromium-cobalt-nickel-molybdenum quaternary system at 1200° C (National Advisory Committee for Aeronautics, 1952), also by Sheldon Paul Rideout and Paul A. Beck (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A survey of stability analysis techniques for automatically controlled aircraft (National Advisory Committee for Aeronautics, 1951), also by Arthur L. Jones and Benjamin R. Briggs (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Synthesis and purification of some alkylbiphenyls and alkylbicyclohexyls (National Advisory Committee for Aeronautics, 1951), also by Irving A. Goodman and Paul H. Wise (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Synthesis of cyclopropane hydrocarbons from methylcyclopropyl ketone. 1. - 2-cyclopropylpropene and 2-cyclopropylpropane (National Advisory Committee for Aeronautics, 1951), also by Vernon A. Slabey and P. H. Wise (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Synthesis of cyclopropane hydrocarbons from methylcyclopropyl ketone. 2. - 2-cyclopropyl-1-pentene, cis and trans 2-cyclopropyl-2-pentene, and 2-cyclopropylpentane (National Advisory Committee for Aeronautics, 1951), also by Vernon A. Slabey and P. H. Wise (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Systematic investigations of the influence of the shape of the profile upon the position of the transition point (NACA, 1947), also by K. Bussmann and A. Ulrich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A tabulation of wind-tunnel pressure data at Mach numbers of 1.61 and 2.01 of five swept wings of the same plan form but different surface shapes (Washington, D.C. : National Advisory Committee for Aeronautics, 1958., 1958), also by Frederick C. Grant and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Technical memorandum - National Advisory Committee for Aeronautics. (National Advisory Committee for Aeronautics, 1920) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Technical memorandums. (Washington., in the 20th century) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Technische Berichte ... (Berlin, 1917), also by Germany. Flugzeugmeisterei der Inspektion der Fliegertruppen (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Temperature distribution in internally heated walls of heat exchangers composed of noncircular flow passages (National Advisory Committee for Aeronautics, 1951), also by E. R. G. Eckert and George M. Low (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Temperature recovery factors on a slender 12À cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45À (NACA, 1955), also by John O. Reller, Frank M. Hamaker, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tensile properties of some sheet materials under rapid-heating conditions (National Advisory Committee for Aeronautics, 1955), also by George J. Heimerl, John E. Inge, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tension properties of aluminum alloys in the presence of stress-raisers. [Part] 1, Effects of triaxial stress states on the fracturing characteristics of 24S-T aluminum alloy (National Advisory Committee for Aeronautics, 1949), also by A. W. Dana, G. Sachs, and E. L. Aul (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tension properties of aluminum alloys in the presence of stress-raisers. [Part] 2, Comparison of notch strength properties of 24S-T, 75S-T, and 24S-T86 aluminum alloy (National Advisory Committee for Aeronautics, 1949), also by E. L. Aul, G. Sachs, and A. W. Dana (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tests in the Variable Density Wind Tunnel to investigate the effects of scale and turbulence on airfoil characteristics (National Advisory Committee for Aeronautics ;, 1931), also by John Stack (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tests of a small-scale NACA submerged inlet at transonic Mach numbers (National Advisory Committee for Aeronautics, 1950), also by L. Stewart Rolls and George A. Rathert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tests of nacelle-propeller combinations in various positions with references to wings IV : thick wing--various radial-engine cowlings--tandem propellers. (National Advisory Committee for Aeronautics, 1934), also by Theodore Theodorsen and Langley Aeronautical Library (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tests of submerged duct installation on a modified fighter airplane in the Ames forty by eighty foot wind tunnel. (National Advisory Committee for Aeronautics, 1947), also by Norman J. Martin and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane (National Advisory Committee for Aeronautics, 1950), also by Leonard Sternfield and Ordway B. Gates (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A theoretical analysis of the effects of fuel motion on airplane dynamics (National Advisory Committee for Aeronautics, 1951), also by Albert A. Schy (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase against maneuvering and nonmaneuvering targets (Washington, D.C. : National Advisory Committee for Aeronautics, [1955], 1955), also by C. H. Woodling, Ordway B. Gates, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas (National Advisory Committee for Aeronautics, 1957), also by Charles C. Graves, Jack S. Grobman, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface (NACA, 1957), also by Virgil E. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow (National Advisory Committee for Aeronautics, 1955), also by Harry L. Runyan, A. Gerald Rainey, and Donald S. Woolston (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds (National Advisory Committee for Aeronautics, 1950), also by John DeYoung (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence (U.S. Government Printing Office, 1957), also by John M. Eggleston and Franklin W. Diederich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical damping in roll and rolling effectiveness of slender cruciform wings (National Advisory Committee for Aeronautics, 1951), also by Gaynor J. Adams (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number (NACA, 1957), also by Virgil E. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical investigation at subsonic speeds of the flow ahead of a slender inclinded parabolic-arc body of revolution and correlation with experimental data obtained at low speeds (National Advisory Committee for Aeronautics, 1954), also by William Letko and Edward C. B. Danforth (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical investigation of drag reduction in maintaining the laminar boundary layer by suction (NACA, 1947), also by A. Ulrich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical investigation of some discontinuous yaw dampers (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by William H. Phillips, Helmut A. Kuehnel, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A theoretical investigation of the drag of generalized aircraft configurations in supersonic flow (NACA, 1957), also by E. W. Graham (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical investigation of transonic similarity for bodies of revolution (National Advisory Committee for Aeronautics, 1950), also by W. Perl and Milton M. Klein (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges (National Advisory Committee for Aeronautics, 1949), also by Frank S. Malvestuto, H. S. Ribner, and Kenneth Margolis (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical loading at supersonic speeds of flat swept-back wings with interacting trailing and leading edges (National Advisory Committee for Aeronautics, 1949), also by Doris Cohen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot (National Advisory Committee for Aeronautics, 1951), also by Ordway B. Gates and Albert A. Schy (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of diborane as a rocket fuel (National Advisory Committee for Aeronautics, 1949), also by Vearl N. Huff, Virginia C. Erdmann, Clyde S. Calvert, and OH) Lewis Flight Propulsion Laboratory (Cleveland (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant : I. Frozen composition (National Advisory Committee for Aeronautics, 1956), also by Vearl N. Huff and Anthony Fortini (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant : II. Equilibrium composition (National Advisory Committee for Aeronautics, 1956), also by Vearl N. Huff, Sanford Gordon, and Anthony Fortini (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant. [Part] I, Frozen composition (National Advisory Committee for Aeronautics, 1956), also by Sanford Gordon, Vearl N. Huff, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines [Part] 3, Liquid ammonia (National Advisory Committee for Aeronautics, 1952), also by Vearl N. Huff, Sanford Gordon, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines [Part] 2, Hydrazine (National Advisory Committee for Aeronautics, 1952), also by Vearl N. Huff, Sanford Gordon, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of liquid ammonia with liquid oxygen as a rocket propellant (National Advisory Committee for Aeronautics, 1958), also by Sanford Gordon (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute (National Advisory Committee for Aeronautics, 1957), also by Anthony Fortine and Vearl N. Huff (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds (National Advisory Committee for Aeronautics, 1954), also by John R. Spreiter and Alberta Alksne (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Sidney M. Harmon (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine (National Advisory Committee for Aeronautics, 1956), also by Vearl N. Huff and Sanford Gordon (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming equilibrium composition (National Advisory Committee for Aeronautics, 1958), also by Sanford Gordon (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow (National Advisory Committee for Aeronautics, 1955), also by M. J. Queijo (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream (National Advisory Committee for Aeronautics, 1947), also by I. E. Garrick and S. I. Rubinow (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical study of the diffusion constant for self-diffusion in metals (National Advisory Committee for Aeronautics, 1949), also by M. Leichter (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds (National Advisory Committee for Aeronautics, 1951), also by John DeYoung (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theoretisch untersuchungen über stationäre potentialströmungen und grenzschichten bei hohen geschwindigkeiten (NACA, 1948), also by K. Oswatitsch and K. Wieghardt (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theories of flow similitude (Government Printing Office, 1928), also by A. F. Zahm (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The theories of turbulence (NACA, 1955), also by L. Agostini and J. Bass (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theory and procedure for determining loads and motions in chine-immersed hydrodynamic impacts of prismatic bodies (National Advisory Committee for Aeronautics, 1952), also by Emanuel Schnitzer and N. Grossman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theory of ignition in nonturbulent and turbulent flow using long-duration discharges (National Advisory Committee for Aeronautics, 1954), also by Clyde C. Swett (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades (U.S. Government Printing Office, 1958), also by Robert F. Coleman and Arnold M. Feingold (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Theory of wing of circular plan form (NACA, 1953), also by N. E. Kochin (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts (National Advisory Committee for Aeronautics, 1950), also by Harvard Lomax, Franklyn B. Fuller, and Max A. Heaslet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Three-dimensional unsteady lift problems in high-speed flight : the triangular wing (National Advisory Committee for Aeronautics, 1951), also by Harvard Lomax, Franklyn B. Fuller, and Max A. Heaslet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Torsion in box wings (National Advisory Committee for Aeronautics ;, 1931), also by John B. Wheatley (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Torsional vibrations of hollow thin-walled cylindrical beams (National Advisory Committee for Aeronautics, 1954), also by Edwin T. Kruszewski and Eldon E. Kordes (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Tracking performance of a swept-wing figher with a disturbed reticle lead-computing sight (Washington, D.C. : National Advisory Committee for Aeronautics, [1955]., 1955), also by Burnett L. Gadeberg, George A. Rathert, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The transformation of heat in an engine (National Advisory Committee for Aeronautics ;, 1929), also by Kurt Neumann (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transient aerodynamic behavior of an airfoil due to different arbitrary modes of nonstationary motions in a supersonic flow (National Advisory Committee for Aeronautics, 1951), also by Chieh-Chien Chang (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles (National Advisory Committee for Aeronautics, 1955), also by Richard J. McCafferty, Richard H. Donlon, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transient behavior of lumped-constant systems for sensing gas pressures (National Advisory Committee for Aeronautics, 1949), also by Gene J. Delio, Richard S. Cesaro, and Glennon V. Schwent (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transient operating characteristics of a turbojet engine when subjected to step changes in fuel flow (National Advisory Committee for Aeronautics, 1950), also by Arthur H. Bell, J. Elmo Farmer, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transition caused by the Laminar flow separation (NACA, 1952), also by T. Maekawa and S. Atsumi (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transonic flow past a wedge profile with detached bow wave : general analytical method and final calculated results (National Advisory Committee for Aeronautics, 1951), also by Walter G. Vincenti and Cleo B. Wagoner (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), also by Charles F. Whitcomb, Harry T. Norton, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A transonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution (National Advisory Committee for Aeronautics, 1957), also by George H. Holdaway, Elaine W. Hatfield, Minor R. Wallace, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transonic wind-tunnel investigation of aerodynamic-loading characteristics of a 2-percent-thick trapezoidal wing in combination with basic and indented bodies (National Advisory Committee for Aeronautics, 1957), also by Thomas C. Kelly (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6 (Washington, D.C. : National Advisory Committee for Aeronautics, [1955], 1955), also by Robert J. Platt, Joseph D. Brooks, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by William E. Palmer, Dale L. Burrows, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Transverse vibrations of hollow thin-walled cylindrical beams (National Advisory Committee for Aeronautics, 1952), also by Bernard Budiansky and Edwin T. Kruszewski (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: True airspeed measurement by ionization-tracer technique (National Advisory Committee for Aeronautics, 1952), also by Bemrose Boyd, George H. Brodie, Robert G. Dorsch, and Lewis Flight Propulsion Laboratory (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation (National Advisory Committee for Aeronautics, 1956), also by Allen J. Metzler, Jack S. Grobman, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Turbulence in the wake of a thin airfoil at low speeds (NACA, 1957), also by George S. Campbell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow (National Advisory Committee for Aeronautics, 1951), also by Maurice Tucker and Stephen H. Maslen (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The twisting effect at transonic speeds of spoiler ailerons on a 45° sweptback, aspect-ratio-4, tapered wing (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Alexander D. Hammond, Jean C. Graven, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Two-dimensional compressible flow in centrifugal compressors with logarithmic-spiral blades (National Advisory Committee for Aeronautics, 1951), also by Gaylord O. Ellis and John D. Stanitz (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Two-dimensional motion of a gas at large supersonic velocities (National Advisory Committee for Aeronautics, 1949), also by S. V. Falkovich (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Two-dimensional transonic flow past airfoils (National Advisory Committee for Aeronautics, 1951), also by Yung-Huai Kuo (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Über die lösung der laminaren grenzschichtgleichung an der ebenen platte für geschwindigkeits- und temperaturfeld bei veränderlichen stoffwerten und für das diffusionsfeld bei höheren konzentrationen (National Advisory Committee for Aeronautics, 1950), also by H. Schuh (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Unsteady oblique interaction of a shock wave with a plane disturbance (National Advisory Committee for Aeronautics, 1953), also by F. K. Moore (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Use of a characteristic surfaces for unsymmetrical supersonic flow problems (National Advisory Committee for Aeronautics, 1949), also by W. E. Moeckel (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The use of a luminescent lacquer for the visual indication of boundary-layer transition (National Advisory Committee for Aeronautics, 1951), also by Jackson R. Stalder and Ellis G. Slack (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Use of Freon-12 as a fluid for aerodynamic testing (National Advisory Committee for Aeronautics ;, 1946), also by Paul W. Huber (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The use of perforated inlets for efficient supersonic diffusion (National Advisory Committee for Aeronautics, 1951), also by John C. Evvard and John W. Blakey (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The use of the horizontal tail for roll control (National Advisory Committee for Aeronautics, 1956), also by John P. Campbell (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Use of truncated flapped airfoils for impingement and icing tests of full-scale leading-edge sections (National Advisory Committee for Aeronautics, 1956), also by U. Von Glahn (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Vapor-fuel-distribution effects on combustion performance of a single tubular combustor (National Advisory Committee for Aeronautics, 1950), also by Richard J. McCafferty and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05 (National Advisory Committee for Aeronautics, 1956), also by James F. Connors, Rudolph C. Meyer, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The Variation in pressure in the cabin of an airplane in flight (National Advisory Committee for Aeronautics ;, 1931), also by Melvin N. Gough (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Variation in smoking tendency among low molecular weight hydrocarbons (National Advisory Committee for Aeronautics, 1952), also by Rose L. Schalla, Glen E. McDonald, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping (National Advisory Committee for Aeronautics, 1949), also by H. E. Moses (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Velocity distributions on symmetrical airfoils in closed tunnels by conformal mapping (National Advisory Committee for Aeronautics, 1948), also by W. Perl and H. E. Moses (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Velocity distributions on two-dimensional wing-duct inlets by conformal mapping (National Advisory Committee for Aeronautics, 1947), also by W. Perl, H. E. Moses, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Vertical and drag ground-reaction forces developed in landing impacts of a large airplane (National Advisory Committee for Aeronautics, 1955), also by Richard H. Sawyer, James M. McKay, and Albert W. Hall (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Visual study of free convection in a narrow vertical enclosure (National Advisory Committee for Aeronautics, 1956), also by E. M. Sparrow, Samuel J. Kaufman, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Visualization of secondary-flow phenomena in blade row (National Advisory Committee for Aeronautics, 1952), also by H. Z. Herzig, G. R. Costello, A. G. Hansen, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A visualization study of secondary flows in cascades (National Advisory Committee for Aeronautics, 1953), also by Arthur G. Hansen, George R. Costello, and Howard Z. Herzig (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems (National Advisory Committee for Aeronautics, 1947), also by Max A. Heaslet, Arthur L. Jones, and Harvard Lomax (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds (National Advisory Committee for Aeronautics, 1953), also by Barrett S. Baldwin, Earl D. Knechtel, John B. Turner, and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime Report A (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime report ... A-. (Washington, 1947) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime report E. (Washington, 1940) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime Report E (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime Report L (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime report. L 1-787. (Washington, 1940) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime report release list. (National Advisory Committee for Aeronautics., 1947) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime Report W (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wartime reports. W. (Washington, D.C., 1946) (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes (National Advisory Committee for Aeronautics, 1955), also by Harvard Lomax and Ames Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel calibration of a combined pitot-static tube and vane-type flow-angularity indicator at Mach numbers of 1.61 and 2.01 (National Advisory Committee for Aeronautics, 1956), also by Archibald R. Sinclair and William D. Mace (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel corrections at high subsonic speeds particularly for an enclosed circular tunnel (NACA, 1952), also by B. Göthert (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6° and NACA 65A006 airfoil section (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Harold S. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by James W. Wiggins and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons (National Advisory Committee for Aeronautics, 1951), also by Harold S. Johnson and John R. Hagerman (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45° sweptback-wing--body combination (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Harold S. Johnson and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of a systematic series of modifications to a flying-boat hull (National Advisory Committee for Aeronautics, 1948), also by Felicien F. Fullmer (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45° high-wing model oscillating in yaw (National Advisory Committee for Aeronautics, 1957), also by Byron M. Jaquet (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane (NACA, 1958), also by Bennie W. Cocke and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps (National Advisory Committee for Aeronautics, 1948), also by Jack D. Brewer and Josephine F. Polhamus (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion (National Advisory Committee for Aeronautics, 1956), also by Thomas R. Turner, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45° sweptback wing at high subsonic speeds (National Advisory Committee for Aeronautics, 1954), also by James W. Wiggins, Richard E. Kuhn, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds, transonic-bump method (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Harold S. Johnson, William C. Hayes, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: WInd-tunnel investigation of the opening characteristics, drag, and stability of several hemispherical parachutes (National Advisory Committee for Aeronautics, 1949), also by Stanley H. Scher and Lawrence J. Gale (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Arthur Henderson (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wind-tunnel research comparing lateral control devices particularly at high angles of attack. III : ordinary ailerons rigged up 10 ̊when neutral (Government Printing Office, 1932), also by Fred E. Weick and Carl J. Wenzinger (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: A wind-tunnel test technique for measuring the dynamic rotary stability derivatives including the cross derivatives at high Mach numbers (National Advisory Committee for Aeronautics, 1955), also by Benjamin H. Beam (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wing-fuselage interference tail buffeting, and air flow about the tail of a low-wing monoplane (Government Printing Office, 1934), also by James A. White and Manely J. Hood (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: Wing tip with subsonic trailing edge (National Advisory Committee for Aeronautics, 1949), also by Harold Mirels, James M. Jagger, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Wire cloth as porous material for transpiration-cooled walls (NACA, 1951), also by E. R. G. Eckert and Lewis Research Center (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Working charts for the determination of the lift distribution between biplane wings (Government Printing Office, 1932), also by Paul Kuhn (page images at HathiTrust; US access only)
• United States. National Advisory Committee for Aeronautics: X-ray diffraction investigation of minor phases of 20 high-temperature alloys (National Advisory Committee for Aeronautics, 1948), also by B. M. Rosenbaum (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: The yawing moment, due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Arthur L. Jones and Alberta Alksne (page images at HathiTrust)
• United States. National Advisory Committee for Aeronautics: Zero-lift drag of a series of bomb shapes at mach numbers from .60 to 1.10 (National Advisory Committee for Aeronautics, 1956), also by William E. Stoney and John Royall (page images at HathiTrust; US access only)

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