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Online Books by

Langley Aeronautical Laboratory

Books from the extended shelves:

• Langley Aeronautical Laboratory: 1.59 and angles of attack up to 36° (National Advisory Committee for Aeronautics, 1952), also by Morton Cooper, Lowell E. Hasel, John P. Gapcynski, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An aerodynamic and hydrodynamic investigation of two multi-jet water-based aircraft having low transonic drag rise (National Advisory Committee for Aeronautics, 1955), also by Roland E. Olson, Ralph P. Bielat, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic characteristics at high speeds of full-scale propellers having different shank designs (National Advisory Committee for Aeronautics, 1947), also by Julian D. Maynard and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms (National Advisory Committee for Aeronautics, 1954), also by William B. Kemp and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic characteristics of a canard-balanced, free-floating, all-movable stabilizer as obtained from rocket-powered-model flight tests and low-speed wind-tunnel tests (National Advisory Committee for Aeronautics, 1953), also by William N. Gardner and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic characteristics of a wing with quarter-chord line swept back 35°, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by William C. Sleeman, William D. Morrison, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 (National Advisory Committee for Aeronautics, 1959), also by Robert W. Dunning, Fred M. Smith, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2° delta wing and an unswept horizontal tail. (National Advisory Committee for Aeronautics, 1958), also by Alan B. Kehlet and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with sliding block for the Mach number range 1.27 to 2.75 (National Advisory Committee for Aeronautics, 1951), also by Paige B. Burbank, Robert W. Byrne, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic loading characteristics in sideslip of a 45° sweptback wing with and without a fence at high subsonic speeds (National Advisory Committee for Aeronautics, 1955), also by Richard E. Kuhn, Andrew L. Byrnes, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Aerodynamic losses in low-pressure tailpipe exhaust ducts for rocket-propelled aircraft (National Advisory Committee for Aeronautics, 1948), also by William K. Hagginbothom, J. G. Thibodaux, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section (National Advisory Committee for Aeronautics, 1952), also by Vernon G. Ward, Merwin D. Pearson, Charles F. Whitcomb, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Air-flow surveys in the vicinity of representative NACA 1-series cowlings (National Advisory Committee for Aeronautics, 1948), also by Robert W. Boswinkle and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. (National Advisory Committee for Aeronautics, 1957), also by Harold L. Crane and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C[sub zeta]₀A₁₀) 10 compressor-blade sections at low speeds (National Advisory Committee for Aeronautics, 1955), also by Melvyn Savage and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An analysis of ducted-airfoil ram jets for supersonic aircraft (National Advisory Committee for Aeronautics, 1948), also by Paul R. Hill, A. A. Gammal, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations (National Advisory Committee for Aeronautics, 1952), also by Joseph Weil, Margaret S. Diederich, George S. Campbell, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An analysis of the normal accelerations and airspeeds of several Lockheed Constellation L-649 airplanes in postwar commercial transport operations over the eastern part of the United States (National Advisory Committee for Aeronautics, 1950), also by Thomas L. Coleman and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel (National Advisory Committee for Aeronautics, 1952), also by Bruce B. Estabrooks and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Analytical and experimental studies of spherical solid-propellant rocket motors (National Advisory Committee for Aeronautics, 1957), also by Joseph G. Thibodaux, George Wright, Robert L. Swain, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems (National Advisory Committee for Aeronautics, 1955), also by Howard J. Curfman, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Langley Aeronautical Laboratory: Application of transonic area rule to a sharp-lipped ducted nacelle (National Advisory Committee for Aeronautics, 1954), also by Richard E. Walters and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Auto-ignition and combustion of diesel fuel in a constant-volume bomb (National Advisory Committee for Aeronautics, 1938), also by Robert F. Selden (page images at HathiTrust)
• Langley Aeronautical Laboratory: Average skin-friction coefficients from boundary-layer measurements on an ogive-cylinder body in flight at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by J. Dan Loposer and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The behavior of beryllium and beryllium copper in a 4,000°F supersonic air jet at a Mach number of 2. (National Advisory Committee for Aeronautics, 1957), also by William H. Kinard and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Bypass-duct design for use with supersonic inlets (National Advisory Committee for Aeronautics, 1956), also by Charles C. Wood, John R. Henry, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Langley Aeronautical Laboratory: Characteristics of airfoils tested in the variable-density tunnel. (National Advisory Committee for Aeronautics, 1938), also by Robert M. Pinkerton and Harry Greenberg (page images at HathiTrust)
• Langley Aeronautical Laboratory: A combined aerodynamic and guidance approach for a simple homing system (National Advisory Committee for Aeronautics, 1953), also by Robert A. Gardiner and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Comparison of ailerons on a rectangular and a tapered wing. (National Advisory Committee for Aeronautics, 1938), also by Hartley A. Soule and William Gracey (page images at HathiTrust)
• Langley Aeronautical Laboratory: Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds (National Advisory Committee for Aeronautics, 1953), also by Robert W. Boswinkle and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade (National Advisory Committee for Aeronautics, 1951), also by Willard R. Westphal, William R. Godwin, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40⁰ sweepback of the 0.27-chord line (National Advisory Committee for Aeronautics, 1949), also by Jones F. Cahill and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings (National Advisory Committee for Aeronautics, 1953), also by Edward J. Radin, Paul J. Carpenter, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed (National Advisory Committee for Aeronautics, 1953), also by A. Richard Felix, James C. Emery, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A compilation of experimental flutter information (National Advisory Committee for Aeronautics, 1954), also by H. J. Cunningham, Brown Harvey H., and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Considerations affecting hydro-ski airplane design (National Advisory Committee for Aeronautics, 1953), also by Kenneth L. Wadlin and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Damping-in-pitch characteristics at high subsonic and transonic speeds of four 35° sweptback wings (National Advisory Committee for Aeronautics, 1953), also by William B. Kemp, Robert E. Becht, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Damping in roll of models with 45°, 60°, and 70° delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models (National Advisory Committee for Aeronautics, 1952), also by E. Claude Sanders and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions (National Advisory Committee for Aeronautics, 1950), also by H. J. Cunningham, R. R. Lundstrom, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Design and evaluation of a turbojet-exhaust simulator with a solid-propellant rocket motor for free-flight research (National Advisory Committee for Aeronautics, 1957), also by Abraham Leiss and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings (1940), also by Abe Silverstein and S. Katzoff (page images at HathiTrust)
• Langley Aeronautical Laboratory: Determination by the free-fall method of the longitudinal stability and control characteristics of a 1/4-scale model of the Bell XS-1 airplane at transonic speeds (National Advisory Committee for Aeronautics, 1948), also by James F. Matthews, Charles W. Mathews, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Determination of profile drag of airplane wing in flight at high Reynolds numbers. (1940), also by Joseph Bicknell (page images at HathiTrust)
• Langley Aeronautical Laboratory: The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 (National Advisory Committee for Aeronautics, 1955), also by B. H. Little, James M. Cubbage, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Discussion of three-dimensional oscillating air forces based on wind-tunnel measurements (National Advisory Committee for Aeronautics, 1953), also by Sherman A. Clevenson, W. J. Tuovila, Sumner A. Leadbetter, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Downwash, sidewash, and wave survey behind a 42⁰ sweptback wing at a Reynolds number of 6.8 x 10⁶ with and without a simulated ground (National Advisory Committee for Aeronautics, 1948), also by G. Chester Furlong, Thomas V. Bollech, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Drag due to lift at Mach numbers up to 2.0 (National Advisory Committee for Aeronautics, 1953), also by Edward C. Polhamus and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Drag measurements at transonic speeds of two bodies of fineness ratio 9 with different locations of maximum body diameter (National Advisory Committee for Aeronautics, 1948), also by Jim Rogers Thompson, Max C. Kurbjun, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect at M = 1.60 of nacelle shape and position on the aerodynamic characteristics in pitch of two wing-body combinations with a 47° sweptback wings (National Advisory Committee for Aeronautics, 1952), also by Lowell E. Hasel, John R. Sevier, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effect of a change in airfoil section on the hinge-moment characteristics of a half-delta tip control with a 60° sweep angle at a Mach number of 6.9 (National Advisory Committee for Aeronautics, 1954), also by David E. Fetterman, Herbert W. Ridyard, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of airfoil profile of symmetrical sections on the low-speed rolling derivatives of 45° sweptback-wing models of aspect ratio 2.61 (National Advisory Committee for Aeronautics, 1949), also by William Letko, Jack D. Brewer, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of compressibility on pressures and forces acting on an airfoil. (1940), also by John Stack, Robert E. Littell, and W. F. Lindsey (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of convergent ejector nozzles on the boattail drag of a 16° conical afterbody at Mach number of 0.6 to 1.26 (National Advisory Committee for Aeronautics, 1958), also by James M. Cubbage and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of downwash on the estimated elevator deflection required for trim of the XS-1 airplane at supersonic speeds (National Advisory Committee for Aeronautics, 1948), also by James T. Matthews and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effect of high solidity on propeller characteristics at high forward speeds from wind-tunnel tests of the NACA 4-(3)(06.3)-06 and NACA 4-(3)(06.4)-09 two-blade propellers (National Advisory Committee for Aeronautics, 1947), also by James B. Delano and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effect of nose radius and shape of the aerodynamic characteristics of a fuselage and a wing-fuselage combination at angles of attack (National Advisory Committee for Aeronautics, 1953), also by John P. Gapcynski, A. Warner Robins, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds (National Advisory Committee for Aeronautics, 1954), also by Carl A. Sandahl, William E. Stoney, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of surface roughness on characteristics of spherical shock waves (National Advisory Committee for Aeronautics, 1955), also by Paul W. Huber, Donald R. McFarland, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of the acceleration of enlongated bodies of revolution upon the resistance in a compressible flow (NACA, 1949), also by F. I. Frankl (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23° conical-diffuser-tail-pipe combination (National Advisory Committee for Aeronautics, 1950), also by Jerome Persh and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 (National Advisory Committee for Aeronautics, 1952), also by Bernard N. Daley, Richard S. Dick, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow (National Advisory Committee for Aeronautics, 1952), also by Eugene S. Love and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects of a sweptback hydrofoil on the force and longitudinal stability characteristics of a typical high-speed airplane (National Advisory Committee for Aeronautics, 1948), also by Raymond B. Wood and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects of aspect ratio on air flow at a high subsonic mach numbers (National Advisory Committee for Aeronautics, 1948), also by W. F. Lindsey, Milton D. Humphreys, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60° sweptback-wing--indented-body configuration at transonic speeds (National Advisory Committee for Aeronautics, 1954), also by Thomas L. Fischetti and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60° delta wing with and without a double slotted flap (National Advisory Committee for Aeronautics, 1953), also by John M. Riebe and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45° sweptback wing of aspect ratio 4 and a 60° delta wing at Mach numbers of 1.41, 1.62, and 1.96 (National Advisory Committee for Aeronautics, 1953), also by Carl R. Jacobsen and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 (National Advisory Committee for Aeronautics, 1952), also by Ross B. Robinson and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45° swept-back wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10⁶ to 4.8 x 10 as determined by pressure distributions, force tests, and calculations (National Advisory Committee for Aeronautics, 1952), also by George L. Pratt and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds (National Advisory Committee for Aeronautics, 1954), also by Harold L. Robinson and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Effects on adjacent surfaces from the firing of rocket jets (National Advisory Committee for Aeronautics, 1957), also by Walter E. Bressette, Abraham Leiss, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Electrical characteristics of spark generators for automotive ignition (National Advisory Committee for Aeronautics, 1926), also by R. B. Brode, F. B. Silsbee, and D. W. Randolph (page images at HathiTrust)
• Langley Aeronautical Laboratory: Error in airspeed measurement due to static-pressure field ahead of an open-nose air-inlet model at transonic speeds (National Advisory Committee for Aeronautics, 1952), also by Thomas C. O'Bryan and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves (National Advisory Committee for Aeronautics, 1949), also by John P. Mayer and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights (National Advisory Committee for Aeronautics, 1951), also by John L. Sewall and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental and theoretical studies of panel flutter at Mach number 1.2 to 3.0 (National Advisory Committee for Aeronautics, 1955), also by Maurice A. Sylvester, Herbert J. Cunningham, Herbert C. Nelson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04 (National Advisory Committee for Aeronautics, 1954), also by Leo T. Chauvin, Joseph P. Maloney, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 (National Advisory Committee for Aeronautics, 1950), also by H. Kurt Strass, Paul E. Purser, E. M. Fields, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60° delta-wing airplane model (National Advisory Committee for Aeronautics, 1958), also by Lewis R. Fisher and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness-chord ratio (National Advisory Committee for Aeronautics, 1955), also by Theodore J. Goldberg and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft (National Advisory Committee for Aeronautics, 1952), also by Charles J. Rodriguez and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail (National Advisory Committee for Aeronautics, 1957), also by Norman S. Land, Annie G. Fox, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41 (National Advisory Committee for Aeronautics, 1954), also by Donald E. Coletti and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental investigation of the mixing loss behind trailing edge of a cascade of three 90° supersonic turning passages (National Advisory Committee for Aeronautics, 1950), also by Luke L. Liccini and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls (National Advisory Committee for Aeronautics, 1954), also by Don D. Davis, George M. Stokes, Thomas B. Sellers, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An experimental study of five annular air inlet configurations at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1953), also by Carroll R. Bryan, Frank F. Fleming, Jospeh R. Milillo, Robert E. Pendley, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An experimental transonic investigation of a 45° sweptback wing-body combination with several types of body indentation with theoretical comparisons included (National Advisory Committee for Aeronautics, 1954), also by Melvin M. Carmel and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experimental verification of the theory of oscillating airfoils (1940), also by Abe Silverstein and U. T. Joyner (page images at HathiTrust)
• Langley Aeronautical Laboratory: Experiments with a model water tunnel (National Advisory Committee for Aeronautics, 1930), also by Eastman N. Jacobs, Ira H. Abbott, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Exploratory investigation of the moments on oscillating control surfaces at transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Dennis J. Martin, C. William Martz, Robert F. Thompson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Exploratory rocket flight tests to investigate the use of a freely spinning monoplane tail for stabilizing a body (National Advisory Committee for Aeronautics, 1952), also by Paul E. Purser, Joseph E. Stevens, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Factors affecting transition at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Archibald R. Sinclair, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flight investigation at high-subsonic, transonic, and supersonic speeds to determine zero-lift drag of fin-stabilized bodies of revolution having fineness ratios of 12.5, 8.91, and 6.04 and varying positions of maximum diameter (National Advisory Committee for Aeronautics, 1949), also by Roger G. Hart, Ellis R. Katz, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A flight investigation of the transonic area rule for a 52.5° sweptback wind-body configuration at Mach numbers between 0.8 and 1.6 (National Advisory Committee for Aeronautics, 1954), also by Sherwood Hoffman and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 (National Advisory Committee for Aeronautics, 1953), also by Clarence A. Brown, Walter E. Bressette, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips (National Advisory Committee for Aeronautics, 1949), also by Walter C. Williams and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flight tests at transonic and supersonic speeds of an airplane-like configuration with a thin straight sharp-edge wings and tail surfaces (National Advisory Committee for Aeronautics, 1957), also by Clarence L. Gillis, Jesse L. Mitchell, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flight tests of a model having self-supporting fuel-carrying panels hinged to the wing tips (National Advisory Committee for Aeronautics, 1949), also by Robert E. Shanks, David C. Grana, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flow of gas through turbine lattices (Langley Memorial Aeronautical Laboratory, 1956), also by M. E. Deĭch and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flutter at very high speeds (National Advisory Committee for Aeronautics, 1957), also by Harry L. Runyan, Homer G. Morgan, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flutter characteristics of swept wings at transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Laurence K. Loftin and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flutter investigation of a true-speed dynamic model with various tip-tank configurations (National Advisory Committee for Aeronautics, 1955), also by John L. Sewall, William B. Igoe, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flutter investigation of two thin, low-aspect-ratio, swept, solid, metal wings in the transonic range by use of free-falling body (National Advisory Committee for Aeronautics, 1952), also by W. T. Lauten, Maurice A. Sylvester, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Flutter of a 60° delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model (National Advisory Committee for Aeronautics, 1952), also by Joseph H. Judd, William T. Lauten, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements (National Advisory Committee for Aeronautics, 1955), also by Eugene D. Schult and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A free-flight investigation of the drag coefficients of two single-engine supersonic interceptor configurations from Mach number 0.8 to 1.90 to determine the effect of inlet and engine locations (National Advisory Committee for Aeronautics, 1955), also by Joseph H. Judd and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine (National Advisory Committee for Aeronautics, 1952), also by Joseph H. Judd, Otto F. Trout, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: General solutions of optimum problems in nonstationary flight (NACA, 1955), also by Angelo Miele and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Heat-transfer measurements in free flight at Mach numbers up to 14.6 on a flat-faced conical nose with a total angle of 29° (National Advisory Committee for Aeronautics, 1958), also by Charles B. Rumsey, Dorothy B. Lee, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Heat transfer to bodies at angles of attack (National Advisory Committee for Aeronautics, 1957), also by William V. Feller and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Improved airplanes windshields to provide vision in stormy weather (National Advisory Committee for Aeronautics, 1937), also by William C. Clay (page images at HathiTrust)
• Langley Aeronautical Laboratory: The influence of directed air flow on combustion in a spark-ignition engine (1940), also by A. M. Rothrock and Robert C. Spencer (page images at HathiTrust)
• Langley Aeronautical Laboratory: Influence of wall boundary layer upon the performance of an axial-flow fan rotor (National Advisory Committee for Aeronautics, 1947), also by Emanuel Boxer and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An initial experimental study of the effect of variations in frequency and impulse on the reduction in temperature recovery factor afforded by large-scale unsteady flow (National Advisory Committee for Aeronautics, 1958), also by Robert R. Howell and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Interaction of moving shocks and hot layers (National Advisory Committee for Aeronautics, 1957), also by Robert V. Hess and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Interrelation of exhaust-gas constituents (National Advisory Committee for Aeronautics, 1938), also by Harold C. Gerrish and Fred Voss (page images at HathiTrust)
• Langley Aeronautical Laboratory: An investigation at Mach numbers 1.94 and 2.41 of jet effects upon the longitudinal and directional stability of a general aircraft configuration employing wing-tip-mounted nacelles (National Advisory Committee for Aeronautics, 1958), also by Frank L. Clark, C. L. W. Edwards, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag (National Advisory Committee for Aeronautics, 1953), also by August F. Bromm, Julia M. Goodwin, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation at transonic speeds of a fixed divergent ejector installed in a single-engine fighter model (National Advisory Committee for Aeronautics, 1958), also by John M. Swihart, Charles E. Mercer, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45° sweptback wing (National Advisory Committee for Aeronautics, 1955), also by Gene J. Bingham and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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.. Lee, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An investigation in the Langley 20-foot free-spinning tunnel of the spin and recovery characteristics of a 1/30-scale model of the Bell X-2 airplane (National Advisory Committee for Aeronautics, 1949), also by Lawrence J. Gale and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of an impulse axial-flow compressor (National Advisory Committee for Aeronautics, 1950), also by John R. Erwin, Wallace M. Schulze, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of an impulse axial-flow compressor rotor over a range of blade angles (National Advisory Committee for Aeronautics, 1950), also by Wallace M. Schulze, Willard R. Westphal, John R. Erwin, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of intake ducts for a high-speed subsonic jet-propelled airplane (National Advisory Committee for Aeronautics, 1947), also by Herbert N. Cohen and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel (National Advisory Committee for Aeronautics, 1952), also by Donald E. Coletti and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: An investigation of the coeffecient of discharge of liquids through small round orifices (U.S. G.P.O., 1926), also by W. F. Joachim (page images at HathiTrust)
• Langley Aeronautical Laboratory: An investigation of the drag characteristics of speed brakes for Mach numbers from 0.20 to 1.30 (National Advisory Committee for Aeronautics, 1958), also by Allan R. Vick and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3 (National Advisory Committee for Aeronautics, 1953), also by Harvey A. Wallskog, Roger G. Hart, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails (National Advisory Committee for Aeronautics, 1949), also by John W. Draper, Robert W. Rose, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the effects of model scale and stream Reynolds number on the aerodynamic characteristics of two rectangular wings at supersonic speeds on the Langley 9-inch supersonic tunnel (National Advisory Committee for Aeronautics, 1955), also by Donald E. Coletti and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the fatigue strength of a full-scale airplane wing structures (National Advisory Committee for Aeronautics, 1951), also by Dwight O. Fearnow and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the NACA 4-(0)(03)-45 two-blade propeller at forward Mach numbers to 0.925 (National Advisory Committee for Aeronautics, 1950), also by Melvin M. Carmel, Joseph R. Milillo, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 (National Advisory Committee for Aeronautics, 1958), also by Roger H. Fournier, H. Norman Silvers, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel (National Advisory Committee for Aeronautics, 1952), also by Eugene S. Love, August F. Bromm, Donald E. Coletti, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of three tapered 45° sweptback cambered and twisted wings covering a simultaneous variation in aspect ratio and thickness ratio and of one related symmetrical wing at transonic speeds by the wing-flow method (National Advisory Committee for Aeronautics, 1953), also by Harold I. Johnson and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of wind-tunnel interference on the downwash behind an airfoil. (National Advisory Committee for Aeronautics, 1937), also by Abe Silverstein and S. Katzoff (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms (National Advisory Committee for Aeronautics, 1953), also by George W. Jones, Hugh C. DuBose, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigation toward simplification of missile control systems (National Advisory Committee for Aeronautics, 1953), also by Howard J. Curfman, Harold L. Crane, H. Kurt Strass, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Investigations at supersonic speeds of the base pressure on bodies of revolution with and without sweptback stabilizing fins (National Advisory Committee for Aeronautics, 1952), also by Eugene S. Love, Robert M. O'Donnell, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Knocking characteristics of aircraft engines. (1940), also by A. M. Rothrock and Arnold E. Biermann (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 (National Advisory Committee for Aeronautics, 1960), also by Robert W. Rainey and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Langley full-scale-tunnel tests of the custer channel wing airplane (NACA, 1953), also by Jerome Pasamanick and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Large-scale flight measurements of zero-lift drag and low-lift drag of 10 wing-body configurations at Mach numbers from 0.8 to 1.6 (National Advisory Committee for Aeronautics, 1953), also by John D. Morrow, Robert L. Nelson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form (National Advisory Committee for Aeronautics, 1955), also by Jim A. Penland, David E. Fetterman, Herbert W. Ridyard, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Load distributions associated with controls at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Douglas R. Lord, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Loads associated with spoilers at supersonic speeds (National Advisory Committee for Aeronautics, 1955), also by Douglas R. Lord, K. R. Czarnecki, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Loads on wings due to spoilers at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Alexander D. Hammond and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Local heat transfer to blunt noses at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by William E. Stoney and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing (National Advisory Committee for Aeronautics, 1952), also by James H. Parks and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 (National Advisory Committee for Aeronautics, 1952), also by Martin T. Moul, Andrew R. Wineman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Longitudinal stability and trim of two rocket-propelled airplane models having 45° sweptback wings and tails with the horizontal tail mounted in two positions (National Advisory Committee for Aeronautics, 1953), also by James H. Parks, Alan B. Kehlet, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Longitudinal stability characteristics at transonic speeds of a rocket-propelled model of an airplane having a 45 degree swept wing of aspect ratio 6.0 (National Advisory Committee for Aeronautics, 1954), also by John C. McFall and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Low-speed cascade investigation of loaded leading-edge compressor blades (National Advisory Committee for Aeronautics, 1956), also by James C. Emery and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Low-speed characteristics in pitch of a 34⁰ sweptforward wing with circular-arc airfoil sections (National Advisory Committee for Aeronautics, 1947), also by D. William Conner, Patrick A. Cancro, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Langley Aeronautical Laboratory: Low-speed pitching derivatives of low-aspect-ratio wings of triangular and modified triangular plan forms (National Advisory Committee for Aeronautics, 1950), also by Alex Goodman, Byron M. Jaquet, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Low-speed static lateral stability characteristics of a canard model having a 60° triangular wing and horizontal tail (National Advisory Committee for Aeronautics, 1949), also by William R. Bates and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Low-speed wind-tunnel investigation of jet control on a 35° swept wing (National Advisory Committee for Aeronautics, 1953), also by John G. Lowry, Thomas R. Turner, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Measurements of aerodynamic heat transfer in turbulent separated regions at a Mach number of 1.8 (National Advisory Committee for Aeronautics, 1958), also by Benjamine J. Garland, J. R. Hall, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane (National Advisory Committee for Aeronautics, 1952), also by Ira P. Jones and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel (National Advisory Committee for Aeronautics, 1953), also by Louis W. Habel, Donald R. Bowman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds (National Advisory Committee for Aeronautics, 1954), also by Robert R. Howell and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A method for the design of porous-wall wind tunnels (National Advisory Committee for Aeronautics, 1956), also by George M. Stokes and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Moment of inertia and damping of fluid in tanks undergoing pitching oscillations (National Advisory Committee for Aeronautics, 1953), also by Edward Widmayer, James R. Reese, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results (National Advisory Committee for Aeronautics, 1953), also by Wallace M. Schulze, George C. Ashby, John R. Erwin, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Robert S. Swanson, E. LaVerne Priddy, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert T. Jones and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Neal Tetervin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by John A. Zalovcik, Clotaire Wood, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Jack Fischel and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Carl F. Schueller, H. Kurt Strass, Peter F. Korycinski, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Charles L. Seacord, Herman O. Ankenbruck, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Marion O. McKinney and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryansky, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Paul Kuhn, Simon H. Diskin, John E. Duberg, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Robert Gottlieb and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Mason F. Miller and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Robert Gottlieb and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Eugene E. Lundquist, W. D. Kroll, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Joseph N. Kotanchik, Robert A. Weinberger, Walter Woods, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Charles M. Zimmey, Viola M. Lappi, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Norman Rafel and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert T. Jones, Harry Greenberg, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by George J. Heimerl, J. Albert Roy, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by S. B. Batdorf, John C. Houbolt, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by I. Elizabeth Garner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by H. S. Ribner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Merven W. Mandel, Leonard M. Bartone, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harry E. Murray, Mary A. Erwin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by J. D. Bird and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by H. S. Ribner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold F. Kleckner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Hubert M. Drake and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold I. Johnson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by W. H. Gray and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John A. Zalovcik, Fred L. Daum, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Norris F. Dow, William A. Hickman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by S. B. Batdorf, Charles Libove, Manuel Stein, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John A. Zalovcik and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Donald D. Baals, Norman F. Smith, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Antonio Ferri and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by I. E. Garrick, Carl Kaplan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Irven Naiman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John L. Crigler and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by A. I. Neihouse and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Clifford S. Gardner, James A. LaHatte, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Blake W. Corson, Mason F. Miller, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Carl Kaplan and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Walter A. Bartlett and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by E. O. Pearson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert B. Liddell and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by F. B. Gustafson, William J. O'Sullivan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Sidney A. Batterson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Marvin Pitkin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Charles W. Mathews, Clotaire Wood, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Walter C. Williams and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Harry Greenberg and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Paul A. Hunter, John P. Reeder, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Irven Naiman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by H. S. Ribner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by I. E. Garrick, Carl Kaplan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Thomas A. Hollingworth and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by S. M. Harmon and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold I. Johnson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Paul E. Purser, Elizabeth G. McKinney, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Marvin Pitkin, Robert O. Schade, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Harold I. Johnson, Joseph R. Vensel, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by William H. Phillips and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert B. Liddell, Vernard E. Lockwood, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by William Mutterperl and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Robert W. Kamm, Frank S. Malvestuto, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Harold F. Kleckner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Robert S. Swanson, Stewart M. Crandall, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John P. Campbell, John W. Paulson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Gerald G. Kayten, William Koven, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Jack Fischel, John M. Riebe, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Thomas A. Hollingworth and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by E. O. Pearson, F. E. West, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Carl A. Sandahl and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Leo F. Fehlner, Robert MacLachlan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Jack Norman Nielsen, Harold H. Sweberg, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Upshur T. Joyner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by F. B. Gustafson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Myron J. Block, S. Katzoff, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John L. Crigler, Herbert W. Talkin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by W. H. Phillips, P. A. Hunter, H. L. Crane, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by William H. Phillips and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John P. Campbell, Charles L. Seacord, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Ray H. Wright and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by De E. Beeler and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by John A. Zalovcik, Fred L. Daum, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Arthur Kantrowitz and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by J. D. Bird and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Chester H. Wolowicz and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Clotaire Wood, John A. Zalovcik, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by M. Leroy Spearman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Thomas A. Toll, Margaret F. Ivey, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by William H. Phillips and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Ralph P. Bielat and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by W. F. Lindsey and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Milton D. Humphreys and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Jerold M. Bidwell, David M. Goldenbaum, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Sidney A. Batterson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Sidney A. Batterson, Thelma Stewart, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Wilbur L. Mayo and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by W. F. Lindsey and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Harry E. Murray, Clarence L. Gillis, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Joseph N. Kotanchik, George W. Zender, Walter Woods, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Douglas A. King, Newton A. Mas, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John M. Riebe, Elizabeth G. McKinney, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Carl F. Schueller, Peter F. Korycinski, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Leo F. Fehlner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Marvin Pitkin, Charles V. Bennett, John W. Draper, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Blake W. Corson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Jerry Goodman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Cloyce E. Matheny and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by J. Ford Johnston, T. J. Voglewede, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Evan H. Schuette and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Walter C. Williams and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Robert Gottlieb, Merven W. Mandel, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1940), also by Eugene E. Lundquist, Joseph N. Kotanchik, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Theodore Theodorsen, Arthur A. Regier, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1941), also by Abe Silverstein, Eugene R. Guryansky, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by W. C. Williams and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Sidney A. Batterson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Marvin Schuldenfrei and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by H. Page Hoggard, Marjorie E. Bulloch, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1941), also by J. M. Nissen, M. D. White, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Eugene E. Lundquist and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Evan H. Schuette, J. Albert Roy, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by S. Katzoff, Robert S. Finn, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by John P. Campbell, Thomas A. Hollingworth, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Robert T. Jones, Joseph W. Wetmore, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by Doris Cohen and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore Theodorsen, Arthur A. Regier, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Theodore 31262081065491Theodorsen (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert S. Swanson, Stewart M. Crandall, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by George J. Heimerl, J. Albert Roy, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John M. Riebe, Oleta Church, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by A. W. Vogeley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by H. A. Pearson, William S. Aiken, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Robert R. Gilruth and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Richard T. Whitcomb and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Marion O. McKinney, Bernard Maggin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), also by F. B. Gustafson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Richard V. Rhode, Philip Donely, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Robert H. Neely, D. William Conner, Richard W. Fairbanks, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Warren A. Tucker, Arthur R. Wallace, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John H. Quinn, Warren A. Tucker, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John A. Zalovcik, Richard B. Skoog, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by John A. Zalovcik and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), also by Laurence K. Loftin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by William J. Underwood, Jones F. Cahill, Albert L. Braslow, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Albert L. Braslow and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Felicien F. Fullmer and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (NACA, in the 1940s), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Albert E. Von Doenhoff, Louis S. Stivers, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), also by Norman S. Land and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by Frank T. Abbott and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by Donald D. Baals, Mary J. Mourhess, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Richard C. Dingeldein, Raymond F. Schaefer, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Harold I. Johnson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1946), also by Hubert M. Drake and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by James P. Peterson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by J. D. Bird and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by James P. Peterson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Myron J. Block, S. Katzoff, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Roy H. Lange and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryanksy, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by F. J. Bailey, F. B. Gustafson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by H. Page Hoggard and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by Paul Kuhn, L. Ross Levin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Francis M. Rogallo, Paul E. Purser, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Harold E. Cleary and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by Harold E. Cleary and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by John G. Lowry, I. Elizabeth Garner, James A. Maloney, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), also by Robert E. Pendley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by James M. Benson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by Merven W. Mandel, Evan H. Schuette, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Isidore G. Recant, Arthur R. Wallace, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by William J. Underwood, Frank T. Abbott, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), also by John W. McKee, Robert B. Liddell, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), also by Ira H. Abbott and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Ira H. Abbott and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by George P. Wood, D. E. Brimley, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), also by John G. Lowry and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), also by John G. Lowry and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by John G. Lowry, Thomas A. Toll, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), also by Isidore G. Recant, Robert S. Swanson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A note on the drag due to lift of delta wings at Mach numbers up to 2.0 (National Advisory Committee for Aeronautics, 1953), also by Robert S. Osborne, Thomas C. Kelly, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: On slender-body theory at transonic speeds (NACA, 1954), also by Keith C. Harder, E. B. Klunker, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Performance characteristics of two 6° and two 12° diffusers at high flow rates (National Advisory Committee for Aeronautics, 1949), also by William J. Nelson, Eileen G. Popp, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Performance of compressor blade cascades at high Mach numbers (National Advisory Committee for Aeronautics, 1947), also by Seymour M. Bogdonoff and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The performance of conical supersonic scoop inlets on circular fuselages (National Advisory Committee for Aeronautics, 1953), also by Lowell E. Hasel and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary evaluation of turbine performance with variable-area turbine nozzles in a turbojet engine (National Advisory Committee for Aeronautics, 1960), also by Carl E. Campbell, Henry J. Welna, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation at low speeds of swept wings in rolling flow (National Advisory Committee for Aeronautics, 1947), also by David Feigenbaum, Alex Goodman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic Mach numbers (National Advisory Committee for Aeronautics, 1953), also by Paul E. Dewey and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation of lithium hydride as a high-temperature internal coolant (National Advisory Committee for Aeronautics, 1957), also by Jerry L. Modisette and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation of self-excited vibrations of single planing surfaces (National Advisory Committee for Aeronautics, 1956), also by Elmo J. Mottard and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation of shock-wave reflections in a small closed ballistic range with various types of walls (National Advisory Committee for Aeronautics, 1952), also by Alexander Peter Sabol and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation of supersonic diffusers (Langley Memorial Aeronautical Laboratory, 1945), also by Arthur Kantrowitz, Coleman duP. Donaldson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 (National Advisory Committee for Aeronautics, 1952), also by K. R. Czarnecki, Archibald R. Sinclair, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigation of the failure of pressurized stiffened cylinders (National Advisory Committee for Aeronautics, 1955), also by Norris F. Dow, Roger W. Peters, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary investigations of strength characteristics of structural elements at elevated temperatures (National Advisory Committee for Aeronautics, 1953), also by Eldon E. Mathauser, Charles Libove, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3 (National Advisory Committee for Aeronautics, 1950), also by Clarence L. Gillis, A. James Vitale, Robert F. Peck, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶ (National Advisory Committee for Aeronautics, 1957), also by J. R. Hall, Robert O. Piland, Katherine C. Speegle, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary results of stability calculations for the bending of box beams with longitudinally stiffened covers connected by posts (National Advisory Committee for Aeronautics, 1952), also by Roger A. Anderson, Aldie E. Johnson, Wilder Thomas W., and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary results of supersonic-jet tests of simplified wing structures (National Advisory Committee for Aeronautics, 1953), also by Richard R. Heldenfels, Richard Rosecrans, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40° sweepback (National Advisory Committee for Aeronautics, 1958), also by Charles T. D'Aiutolo, Homer P. Mason, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary studies of manned satellites wingless configuration : nonlifting (National Advisory Committee for Aeronautics, 1958), also by Maxime A. Faget, James J. Buglia, Benjamine J. Garland, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Preliminary study of some factors which affect the stall-flutter characteristics of thin wings (National Advisory Committee for Aeronautics, 1952), also by A. Gerald Rainey and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A preliminary wind-tunnel investigation of flutter characteristics of delta wings (National Advisory Committee for Aeronautics, 1952), also by Robert W. Herr and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel (National Advisory Committee for Aeronautics, 1950), also by Lowell E. Hasel, Archibald R. Sinclair, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Pressure distribution measurements of the interference effect of the wing on the fuselage at mach numbers of 1.40 and 1.59 (National Advisory Committee for Aeronautics, 1952), also by John P. Gapcynski, United States. National Adviosry Committee for Aeronautics, and James W. Clark (page images at HathiTrust)
• Langley Aeronautical Laboratory: Pressure loads produced on a flat-plate wing by rocket jets exhausting in a spanwise direction below the wing and perpendicular to a free-stream flow of Mach number 2.0 (National Advisory Committee for Aeronautics, 1958), also by Ralph A. Falanga, Joseph J. Janos, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data (National Advisory Committee for Aeronautics, 1952), also by Joseph M. Hallissy and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A proposed ram-jet control system operated by use of diffuser pressure recovery (National Advisory Committee for Aeronautics, 1952), also by Maxime A. Faget and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Recent information on flap and tip controls (National Advisory Committee for Aeronautics, 1953), also by Douglas R. Lord, K. R. Czarnecki, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Recent research on the determination of natural modes and frequencies of aircraft wing structures (National Advisory Committee for Aeronautics, 1956), also by John M. Hedgepeth and United States. National Advisory Committee for Aeronautics. Advisory Group for Aeronautical Research and Development (page images at HathiTrust)
• Langley Aeronautical Laboratory: Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range (National Advisory Committee for Aeronautics, 1952), also by William T. Lauten, Burke R. O'Kelly, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Rocket-powered flight test of a roll-stabilized supersonic missile configuration (National Advisory Committee for Aeronautics, 1950), also by Robert A. Gardiner, Jacob Zarovsky, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Several factors affecting roll control systems of interceptors (National Advisory Committee for Aeronautics, 1953), also by Leonard Sternfield and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form (National Advisory Committee for Aeronautics, 1953), also by Martin Zlotnick, Samuel W. Robinson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Simulation study of a high-performance aircraft including the effect on pilot control of large accelerations during exit and reentry flight (National Advisory Committee for Aeronautics, 1958), also by Robert E. Andrews, Robert A. Champine, James B. Whitten, C. H. Woodling, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 (National Advisory Committee for Aeronautics, 1953), also by Richard I. Sears and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some effects of fin plan form on the static stability of fin-body combinations at Mach number 4.06 (National Advisory Committee for Aeronautics, 1952), also by Edward F. Ulmann, Robert W. Dunning, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds (National Advisory Committee for Aeronautics, 1954), also by Albert G. Few, Thomas J. King, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some experimental studies of panel flutter at Mach number 1.3 (National Advisory Committee for Aeronautics, 1952), also by Maurice A. Sylvester, John E. Baker, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some flutter experiments at a Mach number of 1.3 on cantilever wings with a tubular and closed bodes at the tips (National Advisory Committee for Aeronautics, 1953), also by John Locke McCarty, W. J. Tuovila, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some internal-flow characteristics at zero flight speed of an annular supersonic inlet and an open-nose inlet with sharp and rounded lips (National Advisory Committee for Aeronautics, 1954), also by Joseph R. Milillo and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35° swept-wing model and an unswept-wing model (National Advisory Committee for Aeronautics, 1953), also by Byron M. Jaquet and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some measurements at subsonic speeds of the aerodynamic forces and moments on two delta wings of aspect ratios 2 and 4 oscillating about the midchord (National Advisory Committee for Aeronautics, 1958), also by Sumner A. Leadbetter, Sherman A. Clevenson, United States. National Adviosry Committee for Aeronautics, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some measurements of aerodynamic forces and moments at subsonic speeds on a rectangular wing of aspect ratio 2 oscillating about the midchord (National Advisory Committee for Aeronautics, 1953), also by Edward Widmayer, Sumner A. Leadbetter, Sherman A. Clevenson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some notes on the aerodynamic loads associated with external-store installations (National Advisory Committee for Aeronautics, 1953), also by H. Norman Silvers, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Some observations on loss of static strength due to fatigue cracks (National Advisory Committee for Aeronautics, 1955), also by Walter Illg, Herbert F. Hardrath, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Sound measurements for five shrouded propellers at static conditions (National Advisory Committee for Aeronautics, 1949), also by Harvey H. Hubbard and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Spinning and related problems at high angles of attack for high-speed airplanes (National Advisory Committee for Aeronautics, 1956), also by Walter J. Klinar, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations (National Advisory Committee for Aeronautics, 1952), also by Jesse L. Mitchell and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Studies of the use of Freon-12 as a testing medium in the Langley low-turbulence pressure tunnel (National Advisory Committee for Aeronautics, 1951), also by Albert E. Von Doenhoff, Albert L. Braslow, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A study of the torque equilibrium of an autogiro rotor (1938), also by F. J. Bailey (page images at HathiTrust)
• Langley Aeronautical Laboratory: Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjunction with adjusted hinge-moment parameters (National Advisory Committee for Aeronautics, 1954), also by Harold L. Crane, John M. Elliott, George J. Hurt, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles (National Advisory Committee for Aeronautics, 1951), also by Dennis J. Martin and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A summary of information on support interference at transonic and supersonic speeds (NACA, 1954), also by Eugene S. Love and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Summary of recent theoretical and experimental work on box-beam vibrations (National Advisory Committee for Aeronautics, 1955), also by John M. Hedgepeth, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Surface pressure distributions on a large-scale 49° sweptback wing-body-tail configuration with blowing applied over the flaps and wing leading edge (National Advisory Committee for Aeronautics, 1958), also by H. Clyde McLemore, Marvin P. Fink, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust; US access only)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Telemeter transmission at 219.5 megacycles from two rocket-powered models at Mach number up to 15.7 (National Advisory Committee for Aeronautics, 1958), also by George B. Graves, J. Thomas Markley, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Tensile properties of some sheet materials under rapid-heating conditions (National Advisory Committee for Aeronautics, 1955), also by George J. Heimerl, John E. Inge, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Theoretical analysis of the rolling motions of aircraft using a flicker-type automatic roll stabilization system having a displacement-plus-rate response (National Advisory Committee for Aeronautics, 1949), also by Howard J. Curfman and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface (NACA, 1957), also by Virgil E. Johnson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow (National Advisory Committee for Aeronautics, 1953), also by Harry L. Runyan, A. Gerald Rainey, Donald S. Woolston, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number (NACA, 1957), also by Virgil E. Johnson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Percy J. Bobbitt, Kenneth Margolis, Frank S. Malvestuto, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Three-degree-of-freedom evaluation of the longitudinal transfer functions of a supersonic canard missile configuration including changes in forward speed (National Advisory Committee for Aeronautics, 1954), also by Ernest C. Seaberg and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transient temperature distribution in an aerodynamically heated multiweb wing (National Advisory Committee for Aeronautics, 1953), also by George E. Griffith and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic flight tests to compare the zero-lift drag on underslung and symmetrical nacelles varied chordwise at 40 percent semispan of a 45° sweptback, tapered wing (National Advisory Committee for Aeronautics, 1950), also by William B. Pepper, Sherwood Hoffman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45° sweptback wing (National Advisory Committee for Aeronautics, 1952), also by William B. Pepper, Sherwood Hoffman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic flutter investigation of two 50° semispan modified-delta wings with tip ailerons (National Advisory Committee for Aeronautics, 1958), also by Robert J. Platt and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule (National Advisory Committee for Aeronautics, 1956), also by William E. Palmer, Albert L. Braslow, Robert R. Howell, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail (National Advisory Committee for Aeronautics, 1956), also by Gerald Hieser, Charles F. Reid, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a rocket-propelled airplane model having no horizontal tail (National Advisory Committee for Aeronautics, 1955), also by James H. Parks and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies (National Advisory Committee for Aeronautics, 1953), also by Bruce B. Estabrooks and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45° sweptback wing-body combination (National Advisory Committee for Aeronautics, 1953), also by Melvin M. Carmel and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A transonic wind-tunnel investigation of the effects of nacelles on the aerodynamic characteristics of a complete model configuration (National Advisory Committee for Aeronautics, 1953), also by Melvin M. Carmel, Thomas L. Fischetti, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Transonic wind-tunnel investigation of the interference between a 45° sweptback wing and a systematic series of four bodies (National Advisory Committee for Aeronautics, 1952), also by Donald L. Loving, Dewey E. Wornom, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading (National Advisory Committee for Aeronautics, 1953), also by John R. Erwin, James C. Emery, Melvyn Savage, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of an NACA 23021 airfoil with various arrangements of slotted flaps. (National Advisory Committee for Aeronautics, 1939), also by Carl J. Wenzinger and Thomas A. Harris (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack (National Advisory Committee for Aeronautics, 1956), also by Russell W. McDearmon, Robert A. Jones, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of effect of sweep on rolling derivatives at angles of attack up to 13° and at high subsonic Mach numbers, including a semiempirical method of estimating the rolling derivatives (National Advisory Committee for Aeronautics, 1954), also by James W. Wiggins and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane (NACA, 1958), also by Bennie W. Cocke and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4 (National Advisory Committee for Aeronautics, 1953), also by Paul G. Fournier and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 (National Advisory Committee for Aeronautics, 1953), also by Albert J. Evans, George Liner, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds (National Advisory Committee for Aeronautics, 1957), also by Alexander D. Hammond, Jarrett K. Huffman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: 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 United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow (National Advisory Committee for Aeronautics, 1954), also by Atwood R. Heath, Robert L. O'Neal, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Langley Aeronautical Laboratory: Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series (National Advisory Committee for Aeronautics, 1953), also by Paul G. Fournier, Andrew L. Byrnes, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

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