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United States. National Adviosry Committee for Aeronautics

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• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by William C. Sleeman, Robert E. Becht, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Aerodynamic characteristics of a spoiler-slot-deflector control on a 45° sweptback wing at Mach numbers of 1.61 and 2.01 (National Advisory Committee for Aeronautics, 1957), also by Douglas R. Lord, Robert Moring, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by Boyd C. Myers, Thomas J. King, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds (National Advisory Committee for Aeronautics, 1949), also by Bernard N. Daley, Douglas R. Lord, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 (National Advisory Committee for Aeronautics, 1955), also by Charles B. Rumsey, Russell N. Hopko, Robert O. Piland, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components (National Advisory Committee for Aeronautics, 1950), also by Macon C. Ellis, Carl E. Grigsby, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Air-flow surveys in the vicinity of representative NACA 1-series cowlings (National Advisory Committee for Aeronautics, 1948), also by Robert W. Boswinkle and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by Gareth H. Jordan, Stanley P. Butchart, Earl R. Keener, Flight Research Center (U.S.), and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Altitude performance of an afterburner with pentaborane fuel (National Advisory Committee for Aeronautics, 1957), also by James W. Useller, David B. Fenn, J. Robert Branstetter, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An analog study of a shock-position diffuser control on a supersonic turbojet engine (National Advisory Committee for Aeronautics, 1956), also by David Novik, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Analysis of ram-jet engine performance including effects of component changes (National Advisory Committee for Aeronautics, 1956), also by Richard J. Weber and Roger W. Luidens (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An analysis of ram-jet-engine time delay following a fuel-flow disturbance (National Advisory Committee for Aeronautics, 1955), also by Fred A. Wilcox, Arthur R. Anderson, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Analytical study of the equilibrium thickness of boric oxide deposits on jet-engine surfaces (National Advisory Committee for Aeronautics, 1957), also by Paul C. Setze, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems (National Advisory Committee for Aeronautics, 1955), also by Howard J. Curfman, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• United States. National Adviosry Committee for Aeronautics: Application of oblique-shock sensing system to ram-jet-engine flight Mach number control (National Aeronautics and Space Administration, 1955), also by Fred A. Wilcox, Donald P. Hearth, Lewis Flight Propulsion Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Application of transonic area rule to a sharp-lipped ducted nacelle (National Advisory Committee for Aeronautics, 1954), also by Richard E. Walters and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Average bond energies between boron and elements of the fourth, fifth, sixth, and seventh groups of the periodic table (National Advisory Committee for Aeronautics, 1955), also by A. P. Altshuller, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Blow-out velocities of several slurry and liquid fuels in a 1 7/8-inch-diameter combustor (National Advisory Committee for Aeronautics, 1955), also by James F. Morris, Albert M. Lord, Robert M. Caves, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Bypass-duct design for use with supersonic inlets (National Advisory Committee for Aeronautics, 1956), also by Charles C. Wood, John R. Henry, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane (National Advisory Committee for Aeronautics, 1955), also by John P. Campbell, Carroll H. Woodling, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• United States. National Adviosry Committee for Aeronautics: Chemical and physical factors affecting combustion in fuel : nitric acid systems (National Advisory Committee for Aeronautics, 1958), also by James Baker and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A combined aerodynamic and guidance approach for a simple homing system (National Advisory Committee for Aeronautics, 1953), also by Robert A. Gardiner and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Combustion of aluminum borohydride in a supersonic wind tunnel (National Advisory Committee for Aeronautics, 1955), also by Edward A. Fletcher, Melvin Gerstein, Robert G. Dorsch, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio (National Advisory Committee for Aeronautics, 1958), also by James E. Hatch, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine (National Advisory Committee for Aeronautics, 1957), also by Cavour H. Hauser, William J. Nusbaum, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A compilation of experimental flutter information (National Advisory Committee for Aeronautics, 1954), also by H. J. Cunningham, Brown Harvey H., and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Component performance investigation of J71 experimental turbine. [Part] V, Effect of third stage shrouding on internal-flow conditions of J71-97 turbine (National Advisory Committee for Aeronautics, 1956), also by Donald A. Petrash, Elmer H. Davison, Harold J. Schum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall (National Advisory Committee for Aeronautics, 1955), also by Morgan P. Hanson, Andre J. Meyer, Donald F. Johnson, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Compressor-blade vibration of a J57-P-1 turbojet engine during exploratory operation with inlet-pressure distortions (National Advisory Committee for Aeronautics, 1955), also by Morgan P. Hanson and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Considerations affecting hydro-ski airplane design (National Advisory Committee for Aeronautics, 1953), also by Kenneth L. Wadlin and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Correlation of turbojet combustor carbon formation with smoke-volatility index, smoke point, and NACA K factor (National Advisory Committee for Aeronautics, 1955), also by Edmund R. Jonash, William P. Cook, Helmut F. Butze, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Correlation of turbulent heat transfer in a tube for the dissociating system N204 <==> 2N02. (National Advisory Committee for Aeronautics, 1958), also by Richard S. Brokaw, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Andrew Beke, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Design and experimental investigation of a single-stage turbine with a rotor entering relative Mach number of 2 (National Advisory Committee for Aeronautics, 1958), also by Thomas P. Moffitt and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Design and experimental performance of standard turbine (National Advisory Committee for Aeronautics, 1957), also by Harold E. Rohlik, Herbert W. Scibbe, William T. Wintucky, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Design, over-all performance and stall characteristics (National Advisory Committee for Aeronautics, 1954), also by George W. Lewis, G. K. Serovy, Francis C. Schwenk, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 (National Advisory Committee for Aeronautics, 1956), also by Thomas G. Piercy, Bruce G. Chiccine, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Drag due to lift at Mach numbers up to 2.0 (National Advisory Committee for Aeronautics, 1953), also by Edward C. Polhamus and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine (National Advisory Committee for Aeronautics, 1956), also by Fred A. Wilcox, Paul Whalen, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing (National Advisory Committee for Aeronautics, 1958), also by Edward C. Polhamus, Kenneth P. Spreemann, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of a reduction in stator solidity on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, R. Y. Wong, Warner L. Stewart, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of annular inlet baffles on rotating stall, blade vibration, and performance of an axial-flow compressor in a turbojet engine (National Advisory Committee for Aeronautics, 1955), also by Johnson,Donald F., Morgan P. Hanson, Andre J. Meyer, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), also by Charles F. Zalabak, Arthur N. Curren, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of centerbody boundary-layer removal near the throat of three conical nose inlets at mach 1.6 to 2.0 (National Advisory Committee for Aeronautics, 1955), also by Emil J. Kremzier, George A. Wise, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of circumferential total-pressure gradients typical of single-inlet duct installations on performance of an axial-flow turbojet engine (National Advisory Committee for Aeronautics, 1955), also by S. C. Huntley, Curits L. Walker, Joseph N. Sivo, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), also by Arthur N. Curren, Charles F. Zalabak, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of fuel drop size and injector configuration on screaming in a 200-pound-thrust rocket engine using liquid oxygen and heptane (National Advisory Committee for Aeronautics, 1958), also by Charles E. Feiler and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of high rotor pressure-surface diffusion on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1955), also by James W. Miser, Daniel E. Monroe, Warner L. Stewart, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of plastic viscosity and yield value on spray characteristics of magnesium-slurry fuel (National Advisory Committee for Aeronautics, 1957), also by George M. Prok and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of surface roughness on characteristics of spherical shock waves (National Advisory Committee for Aeronautics, 1955), also by Paul W. Huber, Donald R. McFarland, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of wing-mounted external stores on the lift and drag of the Douglas D-558-II research airplane at transonic speeds (National Advisory Committee for Aeronautics, 1957), also by Jack Nugent and Flight Research Center (U.S.) (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effect of yaw and angle of attack on pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71 (National Advisory Committee for Aeronautics, 1954), also by Raymond J. Comenzo, Ernest A. Mackley, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4 (National Advisory Committee for Aeronautics, 1954), also by Homer P. Mason, Allen B. Henning, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds (National Advisory Committee for Aeronautics, 1956), also by Frank S. Malvestuto, William J. Alford, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Effects on adjacent surfaces from the firing of rocket jets (National Advisory Committee for Aeronautics, 1957), also by Walter E. Bressette, Abraham Leiss, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Engine performance of overtemperature heat-treated S-816 buckets (National Advisory Committee for Aeronautics, 1956), also by Robert A. Signorelli, F. B. Garrett, John W. Weeton, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Estimation of specific surface of fine divided magnesium (National Advisory Committee for Aeronautics, 1956), also by Murray L. Pinns and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An evaluation of electropolished and nonelectropolished blades of alloys refractaloy 26, M-252, and waspaloy in a J33-9 turbojet engine (National Advisory Committee for Aeronautics, 1955), also by Francis Jacob Clauss, J. R. Johnston, R. A. Signorelli, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Evaluation of the use of electrical resistance for detecting overtemperatured S-816 turbine blades (National Advisory Committee for Aeronautics, 1957), also by Leonard Robins, Lewis A. Rodert, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers (National Advisory Committee for Aeronautics, 1957), also by John A. Moore, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Experimental investigation at Mach numbers 1.88, 3.16, and 3.83 of pressure drag of wedge diverters simulating boundary-layer-removal systems for side-inlets (National Advisory Committee for Aeronautics, 1954), also by Thomas G. Piercy, Harry W. Johnson, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Experimental investigation of direct control of diffuser pressure on 16-inch ram-jet engine (National Advisory Committee for Aeronautics, 1955), also by William R. Dunbar, Herbert G. Hurrell, George Vasu, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Experimental investigation of external water-spray cooling in a turbojet engine utilizing several injection configurations including orifices in the rotor-blade bases (National Advisory Committee for Aeronautics, 1955), also by Roy A. McKinnon, John C. Freche, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients (National Advisory Committee for Aeronautics, 1952), also by Loren A. Beatty, James C. Emery, Melvyn Savage, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Robert R. Howell, Albert L. Braslow, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Fabrication and endurance of air-cooled strut-supported turbine blades with struts cast of X-40 alloy (National Advisory Committee for Aeronautics, 1956), also by Eugene F. Schum, Robert E. Oldrieve, Francis S. Stepka, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Factors affecting the maximum lift-drag ratio at high supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Charles H. McLellan, Robert W. Dunning, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Factors affecting transition at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Archibald R. Sinclair, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Five organo-metallic additives (National Advisory Committee for Aeronautics, 1955), also by Edmund R. Jonash, William P. Cook, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method (National Advisory Committee for Aeronautics, 1950), also by Jim Rogers Thompson, George E. Cooper, Richard S. Bray, and Ames Research Center (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8 (National Advisory Committee for Aeronautics, 1956), also by Leonard W. Putland, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8 (National Advisory Committee for Aeronautics, 1951), also by R. I. Sears, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds (National Advisory Committee for Aeronautics, 1958), also by Gene J. Matranga, Katharine H. Armistead, and Flight Research Center (U.S.) (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift (National Advisory Committee for Aeronautics, 1950), also by John D. Morrow, Ellis Katz, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1 (National Advisory Committee for Aeronautics, 1957), also by Walter A. Bartlett, Charles F. Merlet, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A flow calorimeter for determining combustion efficiency from residual enthalpy of exhaust gases (National Advisory Committee for Aeronautics, 1954), also by Albert Evans, Robert R. Hibbard, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flutter at very high speeds (National Advisory Committee for Aeronautics, 1957), also by Harry L. Runyan, Homer G. Morgan, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flutter characteristics of swept wings at transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Laurence K. Loftin and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model (National Advisory Committee for Aeronautics, 1956), also by Albert P. Martina, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50 (National Advisory Committee for Aeronautics, 1955), also by Ralph A. Falanga, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration (National Advisory Committee for Aeronautics, 1955), also by Charles B. Rumsey, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Fuel characteristics pertinent to the design of aircraft fuel systems. Supplement 1 - Additional information on MIL-F-7914(AER) Grade JP-5 fuel and several fuel oils (National Advisory Committee for Aeronautics, 1953), also by Henry C. Barnett, Robert R. Hibbard, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Heat of combustion of the product formed by the reaction of diborane and an unsaturated hydrocarbon (LFPL-MZ-2) (National Advisory Committee for Aeronautics, 1953), also by Harrison Allen and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0 (National Advisory Committee for Aeronautics, 1958), also by J. Thomas Markley, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Heat transfer to bodies at angles of attack (National Advisory Committee for Aeronautics, 1957), also by William V. Feller and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region (National Advisory Committee for Aeronautics, 1955), also by Harold B. Pierce, Thomas D. Reisert, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An inlet design concept to reduce flow distortion at angle of attack (National Advisory Committee for Aeronautics, 1957), also by Carl F. Schueller, Leonard E. Stitt, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics (National Advisory Committee for Aeronautics, 1956), also by H. George Krull, William T. Beale, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Internal performance of several divergent-shroud ejector nozzles with high divergence angles (National Advisory Committee for Aeronautics, 1957), also by Arthur M. Trout, John H. Povolny, S. Stephen Papell, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45° sweptback highly tapered wing in combination with basic and indented bodies (National Advisory Committee for Aeronautics, 1957), also by Thomas L. Fischetti, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles (National Advisory Committee for Aeronautics, 1956), also by Donald P. Hearth, Robert W. Cubbison, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination (National Advisory Committee for Aeronautics, 1958), also by J. Cary Nettles, Robert C. Campbell, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of a simple device for preventing separation due to shock and boundary-layer interaction (National Advisory Committee for Aeronautics, 1950), also by Coleman duP. Donaldson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air (National Advisory Committee for Aeronautics, 1957), also by James F. Connors, Rudolph C. Meyer, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of an impulse axial-flow compressor (National Advisory Committee for Aeronautics, 1950), also by John R. Erwin, Wallace M. Schulze, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 (National Advisory Committee for Aeronautics, 1958), also by Richard A. Yeager, Laurence W. Gertsma, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of effect of fluoride on corrosion of 2S-0 aluminum and 347 stainless steel in fuming nitric acid a t 170° (National Advisory Committee for Aeronautics, 1954), also by Charles E. Feiler, Gerald Morrell, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds (National Advisory Committee for Aeronautics, 1958), also by Abraham Leiss, Walter J. Kouyoumjian, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of intake ducts for a high-speed subsonic jet-propelled airplane (National Advisory Committee for Aeronautics, 1947), also by Herbert N. Cohen and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2 (National Advisory Committee for Aeronautics, 1950), also by Robert E. Pendley, Harold L. Robinson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of shock : boundary-layer interaction on the spike of a conical-spike nose inlet (National Advisory Committee for Aeronautics, 1957), also by George A. Wise, William H. Sterbentz, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord (National Advisory Committee for Aeronautics, 1954), also by Mitchel H. Bertram, William D. McCauley, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the aerodynamic characteristics in pitch and sideslip of a 45° swept-wing airplane configuration with various vertical locations of the wing and horizontal tail. Static lateral and directional stability ; Mach numbers of 1.41 and 2.01 (National Advisory Committee for Aeronautics, 1957), also by M. Leroy Spearman, Ross B. Robinson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45° sweptback wing-body configuration at transonic speeds (National Advisory Committee for Aeronautics, 1954), also by Claude V. Williams, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the fatigue strength of a full-scale airplane wing structures (National Advisory Committee for Aeronautics, 1951), also by Dwight O. Fearnow and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million (National Advisory Committee for Aeronautics, 1954), also by Thomas N. Canning and Ames Research Center (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925 (National Advisory Committee for Aeronautics, 1949), also by James B. Delano, Francis G. Morgan, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925 (National Advisory Committee for Aeronautics, 1949), also by James B. Delano, Daniel E. Harrison, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes (National Advisory Committee for Aeronautics, 1955), also by Ray E. Budinger, Harold R. Kaufman, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6 (National Advisory Committee for Aeronautics, 1957), also by George W. Jones, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5. [Part] I, , Velocity-diagram study (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, Warner L. Stewart, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigation toward simplification of missile control systems (National Advisory Committee for Aeronautics, 1953), also by Howard J. Curfman, Harold L. Crane, H. Kurt Strass, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles (National Advisory Committee for Aeronautics, 1949), also by Eugene S. Love, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35°, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1950), also by Robert F. Thompson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane 45° swept-back wing of aspect ratio 3, taper ratio 0.4 with 3-percent-thick, biconvex section (National Advisory Committee for Aeronautics, 1951), also by John C. Heitmeyer and Ames Research Center (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Load distributions associated with controls at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Douglas R. Lord, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Loads associated with spoilers at supersonic speeds (National Advisory Committee for Aeronautics, 1955), also by Douglas R. Lord, K. R. Czarnecki, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Loads on wings due to spoilers at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Alexander D. Hammond and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Local heat transfer to blunt noses at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by William E. Stoney and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Low-pressure performance of different diameter experimental combustor liners (National Advisory Committee for Aeronautics, 1954), also by Ralph T. Dittrich and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Low-speed cascade investigation of loaded leading-edge compressor blades (National Advisory Committee for Aeronautics, 1956), also by James C. Emery and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A low-speed investigation of a thin 60° delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size (National Advisory Committee for Aeronautics, 1955), also by Delwin R. Croom, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing (National Advisory Committee for Aeronautics, 1950), also by Arvid L. Keith, Jack Schiff, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A method for determining core dimensions of heat exchanger with one dominating film resistance and verification with experimental data (National Advisory Committee for Aeronautics, 1957), also by John N. B. Livingood, Anthony J. Diaguila, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A method for determining turbine design characteristics for rocket turbodrive applications (National Advisory Committee for Aeronautics, 1958), also by Warner L. Stewart, Warren J. Whitney, David G. Evans, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A method for the design of porous-wall wind tunnels (National Advisory Committee for Aeronautics, 1956), also by George M. Stokes and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds (National Advisory Committee for Aeronautics, 1952), also by Paul E. Purser, Jesse L. Mitchell, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Nine oxygen-bearing compounds (National Advisory Committee for Aeronautics, 1956), also by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05 (National Advisory Committee for Aeronautics, 1954), also by Edward F. Ulmann, Robert W. Dunning, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Performance comparisons of JFC-2 and MIL-F-5624A (JP-3) fuels in tubular and annular combustors (National Advisory Committee for Aeronautics, 1952), also by Richard J. McCafferty and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Performance of a translating-double-cone axisymmetric inlet with cowl bypass at mach number from 2.0 to 3.5 (National Advisory Committee for Aeronautics, 1957), also by James F. Connors, GeorgeA. Wise, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Performance of compressor blade cascades at high Mach numbers (National Advisory Committee for Aeronautics, 1947), also by Seymour M. Bogdonoff and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: The performance of conical supersonic scoop inlets on circular fuselages (National Advisory Committee for Aeronautics, 1953), also by Lowell E. Hasel and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight. [Part] I, U-shaped channel walls for secondary-air entry / (National Advisory Committee for Aeronautics, 1955), also by Eugene V. Zettle, Robert Friedman, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0 (National Advisory Committee for Aeronautics, 1957), also by Paul C. Simon, Ronald G. Huff, Dennis W. Brown, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Performance of pure fuels in a single J33 combustor. [Part] III, Five hydrocarbon gaseous fuels and one oxygenated-hydrocarbon gaseous fuel (National Advisory Committee for Aeronautics, 1956), also by Arthur L. Smith, Jerrold D. Wear, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A pivoting-cowl-and-spike technique for efficient angle-of-attack operation of supersonic inlets (National Advisory Committee for Aeronautics, 1958), also by Nick E. Samanich and Robert W. Cubbison (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Position errors of the service airspeed installations of 10 airplanes (National Advisory Committee for Aeronautics, 1949), also by William Gracey (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary attempts at isothermal compression of a supersonic air stream (National Advisory Committee for Aeronautics, 1956), also by E. Perchonok, F. Wilcox, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation at low speeds of swept wings in rolling flow (National Advisory Committee for Aeronautics, 1947), also by David Feigenbaum, Alex Goodman, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of a variable Mach number two-dimensional supersonic tunnel of fixed geometry (National Advisory Committee for Aeronautics, 1949), also by William J. Nelson, Frederick Bloetscher, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of hollow-bladed turbines having closed and open blade tips (National Advisory Committee for Aeronautics, 1955), also by Gordon T. Smith, Robert O. Hickel, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of lithium hydride as a high-temperature internal coolant (National Advisory Committee for Aeronautics, 1957), also by Jerry L. Modisette and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of self-excited vibrations of single planing surfaces (National Advisory Committee for Aeronautics, 1956), also by Elmo J. Mottard and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet (National Advisory Committee for Aeronautics, 1957), also by Milton A. Beheim, Thomas G. Piercy, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of the compressive strength and creep lifetime of 2024-T3 (formerly 24S-T3) aluminum-alloy plates at elevated temperatures (National Advisory Committee for Aeronautics, 1955), also by Eldon E. Mathauser, William D. Deveikis, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary investigation of the failure of pressurized stiffened cylinders (National Advisory Committee for Aeronautics, 1955), also by Norris F. Dow, Roger W. Peters, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary results of supersonic-jet tests of simplified wing structures (National Advisory Committee for Aeronautics, 1953), also by Richard R. Heldenfels, Richard Rosecrans, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preliminary studies of rolling-contact fatigue life of high-temperature bearing materials (National Advisory Committee for Aeronautics, 1958), also by Thomas L. Carter, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A preliminary wind-tunnel investigation of flutter characteristics of delta wings (National Advisory Committee for Aeronautics, 1952), also by Robert W. Herr and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preparation and handling of magnesium-hydrocarbon slurries for jet-engine applications (National Advisory Committee for Aeronautics, 1955), also by Henry C. Barnett, Paul H. Wise, Albert M. Lord, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preparation of 50 percent boron-hydrocarbon slurries using combinations of glycerol sorbitan laurate with various thickeners (National Advisory Committee for Aeronautics, 1955), also by Irving A. Goodman, Virginia O. Fenn, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Preparation of dipentaborylmethane by Friedel-Crafts reaction (National Advisory Committee for Aeronautics, 1958), also by Albert C. Antoine, Lewis Flight Propulsion Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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, Langley Aeronautical Laboratory, and James W. Clark (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: The problem of the turbo-compressor (National Advisory Committee for Aeronautics, 1920), also by Ren©Øe Devillers (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: The rate of decomposition of liquid pentaborane from 85⁰ to 202⁰ C (National Advisory Committee for Aeronautics, 1955), also by Glen E. McDonald and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Recent information on flap and tip controls (National Advisory Committee for Aeronautics, 1953), also by Douglas R. Lord, K. R. Czarnecki, and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range (National Advisory Committee for Aeronautics, 1951), also by WIlliam T. Lauten, Herbert C. Nelson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Review of the toxicological properties of pentaborane, diborane, decaborane, and boric acid (National Advisory Committee for Aeronautics, 1956), also by Joseph M. Lamberti and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Edward C. Polhamus, William C. Sleeman, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor (National Advisory Committee for Aeronautics, 1954), also by Robert W. Graham, Vasily D. Prian, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Self-ignition temperatures and flash points of some high-energy fuels (National Advisory Committee for Aeronautics, 1957), also by Barbara Pusanski and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Several factors affecting roll control systems of interceptors (National Advisory Committee for Aeronautics, 1953), also by Leonard Sternfield and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver (National Advisory Committee for Aeronautics, 1956), also by Leonard Sternfield, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Simulated afterburner performance with hydrogen peroxide injection for thrust augmentation (National Advisory Committee for Aeronautics, 1956), also by Allen J. Metzler, Jack S. Grobman, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing (National Advisory Committee for Aeronautics, 1954), also by Roland D. English, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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, Langley Aeronautical Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Some notes on the aerodynamic loads associated with external-store installations (National Advisory Committee for Aeronautics, 1953), also by H. Norman Silvers, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Some observations on loss of static strength due to fatigue cracks (National Advisory Committee for Aeronautics, 1955), also by Walter Illg, Herbert F. Hardrath, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Some recent research on the handling qualities of airplanes (National Advisory Committee for Aeronautics, 1956), also by Walter C. Williams, William H. Phillips, Flight Research Center (U.S.), and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Sound measurements for five shrouded propellers at static conditions (National Advisory Committee for Aeronautics, 1949), also by Harvey H. Hubbard and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Span loadings due to wing twist at transonic and supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by Frederick C. Grant, John P. Mugler, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Spinning and related problems at high angles of attack for high-speed airplanes (National Advisory Committee for Aeronautics, 1956), also by Walter J. Klinar, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Spontaneous ignition limits of pentaborane (National Advisory Committee for Aeronautics, 1957), also by Rose L. Schalla and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Spontaneous ignition of pentaborane sprays in a hot-air stream (National Advisory Committee for Aeronautics, 1956), also by Erwin A. Lezberg, Albert M. Lord, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4 (National Advisory Committee for Aeronautics, 1957), also by Reginald R. Lundstrom, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations (National Advisory Committee for Aeronautics, 1952), also by Jesse L. Mitchell and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine (National Advisory Committee for Aeronautics, 1955), also by Reeves P. Cochran, Robert P. Dengler, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Strategic virgin metal requirements for five aircraft gas turbine engines (National Advisory Committee for Aeronautics, 1949), also by United States. National Advisory Committee for Aeronautics. Subcommittee on Heat Resisting Materials (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A study of liquid boric oxide particle growth rates in a gas stream from a simulated jet engine combustor (National Advisory Committee for Aeronautics, 1957), also by Paul C. Setze, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A study of the response of panels to random acoustic excitation (National Advisory Committee for Aeronautics, 1955), also by R. W. Hess, Harvey H. Hubbard, Leslie W. Lassiter, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957 (National Advisory Committee for Aeronautics, 1958), also by Martin R. Copp, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Summary of recent theoretical and experimental work on box-beam vibrations (National Advisory Committee for Aeronautics, 1955), also by John M. Hedgepeth, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model (National Advisory Committee for Aeronautics, 1954), also by William T. Lauten, Joseph H. Judd, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust; US access only)
• United States. National Adviosry Committee for Aeronautics: Survey of hydrogen combustion properties (National Advisory Committee for Aeronautics, 1957), also by Isadore L. Drell, Frank E. Belles, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A survey of methods for turbojet thrust measurement applicable to flight installation (National Advisory Committee for Aeronautics, 1955), also by William A. Fleming, David S. Gabriel, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A temperature-schedule acceleration control for a turbojet engine and its use with a speed control (National Advisory Committee for Aeronautics, 1957), also by Theodore F. Gerus, Herbert J. Heppler, Albert G. Powers, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Tensile properties of some sheet materials under rapid-heating conditions (National Advisory Committee for Aeronautics, 1955), also by George J. Heimerl, John E. Inge, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas (National Advisory Committee for Aeronautics, 1957), also by Charles C. Graves, Jack S. Grobman, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities (National Advisory Committee for Aeronautics, 1956), also by William J. Alford (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant. [Part] I, Frozen composition (National Advisory Committee for Aeronautics, 1956), also by Sanford Gordon, Vearl N. Huff, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition (National Advisory Committee for Aeronautics, 1957), also by Sanford Gordon, Kenneth S. Drellishak, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Torsion, compression, and bending tests of tubular sections machines from 75S-T6 rolled round rod (National Advisory Committee for Aeronautics, 1952), also by R. L. Moore, J. W. Clark, and Aluminum Company of America (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles (National Advisory Committee for Aeronautics, 1955), also by Richard J. McCafferty, Richard H. Donlon, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Transient temperature distribution in an aerodynamically heated multiweb wing (National Advisory Committee for Aeronautics, 1953), also by George E. Griffith and Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation (National Advisory Committee for Aeronautics, 1956), also by Allen J. Metzler, Jack S. Grobman, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05 (National Advisory Committee for Aeronautics, 1956), also by James F. Connors, Rudolph C. Meyer, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Visual study of free convection in a narrow vertical enclosure (National Advisory Committee for Aeronautics, 1956), also by E. M. Sparrow, Samuel J. Kaufman, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion (National Advisory Committee for Aeronautics, 1956), also by Thomas R. Turner, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45° sweptback wing at high subsonic speeds (National Advisory Committee for Aeronautics, 1954), also by James W. Wiggins, Richard E. Kuhn, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)
• United States. National Adviosry Committee for Aeronautics: 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 Langley Aeronautical Laboratory (page images at HathiTrust)

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