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Filed under: Aeronautics -- Research- Résumé des principaux travaux exécutés pendant la guerre au Laboratoire aérodynamique Eiffel, 1915-1918 (Librairie aéronautique, E. Chiron, éditeur, 1919), by Gustave Eiffel (page images at HathiTrust; US access only)
- Motion devices for linear and angular oscillation and for abrupt acceleration studies on human subjects (impact), a description of facilities in use and proposed (National Academy of Sciences-National Research Council, 1961), by Henning E. von Gierke, Eugene Steinmetz, and Armed Forces-NRC Committee on Bio-astronautics (page images at HathiTrust)
- Aerospace thesis topics list; research problems for science & engineering students. (Minta Martin Aeronautical Student Fund of the AIAA, 1963), by Institute of the Aerospace Sciences. Engineers Career Development Committee (page images at HathiTrust)
- Office of Aerospace Research progress (The Office, in the 20th century), by Jacob Seiden and United States. Air Force. Office of Aerospace Research (page images at HathiTrust)
- Report. (London, 1909), by Aeronautical Research Council (Great Britain) and Great Britain Advisory Committee for Aeronautics (page images at HathiTrust)
- A preliminary determination of normal accelerations on racing airplanes (National Advisory Committee for Aeronautics, 1935), by Nathan F. Scudder, H. W. Kirschbaum, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Notes on the technique of landing airplanes equipped with wing flaps (National Advisory Committee for Aeronautics, 1936), by Melvin N. Gough and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A study of the factors affecting the range of airplanes (National Advisory Committee for Aeronautics, 1937), by David Beirmann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Generalized analysis of experimental observations in problems of elastic stability (National Advisory Committee for Aeronautics, 1938), by Eugene E. Lundquist and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Some elementary principles of shell stress analysis with notes on the use of the shear center (National Advisory Committee for Aeronautics, 1939), by Paul Kuhn and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- An experimental investigation of the normal acceleration of an airplane model in a gust (National Advisory Committee for Aeronautics, 1939), by Philip Donely and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A semi-graphical method for analyzing strains measured on three or four gage lines intersecting at 45 degrees (National Advisory Committee for Aeronautics, 1939), by H. N. Hill and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Bending stresses due to torsion in cantilever box beams (National Advisory Committee for Aeronautics, 1935), by Paul Kuhn and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Principal effects of axial load on moment-distribution analysis of rigid structures (National Advisory Committee for Aeronautics, 1935), by Benjamin Wylie James and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Compressive tests of a monocoque box (National Advisory Committee for Aeronautics, 1939), by Walter Ramberg, Samuel Levy, Albert E. McPherson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Limitations of the pilot in applying forces to airplane controls (National Advisory Committee for Aeronautics, 1936), by Melvin N. Gough, A. P. Beard, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Spin tests of two models of a low-wing monoplane to investigate scale effect in the model test range (National Advisory Committee for Aeronautics, 1941), by Charles J. Donlan and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The development of electrical strain gages (National Advisory Committee for Aeronautics, 1940), by A. V. De Forest, H. Leaderman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The organization, research activities and facilities of the NACA. ([Washington], 1948), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- In-flight simulation, theory and application (Cornell Aeronautical Laboratory, 1961), by Edwin A. Kidd, Robert P. Harper, and Gifford Bull (page images at HathiTrust)
- Report of an inspection of certain European hydromechanical and aeromechanical test and research facilities during October-December 1945. (Washington, 1949), by Harold Eugene Saunders (page images at HathiTrust; US access only)
- Research in aeronautics and space. (Langley Research Center, 1971), by Langley Research Center (page images at HathiTrust)
- Investigations in Soviet hypervelocity testing technique; comprehensive report ([Washington], 1965), by Library of Congress. Aerospace Technology Division and Alexis Baratoff (page images at HathiTrust)
- Technical project descriptions, active. (Buffalo, 1951), by Cornell Aeronautical Laboratory (page images at HathiTrust)
- Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Thomas F. Gelder and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- A theoretical analysis of simulated transonic boundary layers in cryogenic-nitrogen wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Jerry B. Adcock, Charles B. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Support interference of wind tunnel models : a selective annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Marie H. Tuttle, Blair B. Gloss, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
- A unique facility for V/STOL aircraft hover testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Richard G. Culpepper, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and United States. Naval Air Systems Command (page images at HathiTrust)
- Empirically determined wind and scale effects on hot gas recirculation characteristics of jet V/Stol aircraft (National Aeronautics and Space Administration, 1969), by Patrick E. Ryan, Wayne J. Cosgrove, Bell Aerospace Corporation. Bell Aerosystems Company, and Langley Research Center (page images at HathiTrust; US access only)
- NASA TN D-5335 (National Aeronautics and Space Administration ;, 1969), by James A. Blackwell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- NASA TN D-5369 (National Aeronautics and Space Administration ;, 1969), by Arthur G. Holms, Steven M. Sidik, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Probability concepts applied to sequential equipment operation (National Aeronautics and Space Administration ;, 1971), by Lamar Layton, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), by H. S. Ribner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), by H. S. Ribner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by John A. Zalovcik, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Irven Naiman, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by John L. Crigler, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), by A. I. Neihouse, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), by Clifford S. Gardner, James A. LaHatte, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Robert B. Liddell, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by F. B. Gustafson, William J. O'Sullivan, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Sidney A. Batterson, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), by Charles W. Mathews, Clotaire Wood, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), by Paul A. Hunter, John P. Reeder, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Irven Naiman, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), by H. S. Ribner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by M. Leroy Spearman, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), by Sidney A. Batterson, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), by Sidney A. Batterson, Thelma Stewart, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes (NACA, 1944), by Marvin Pitkin, Bernard Maggin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by John M. Riebe, Elizabeth G. McKinney, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- On the determination of certain basic types of supersonic flow fields (NACA, 1954), by Carlo Ferrari and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Further measurements of normal accelerations on racing airplanes (National Advisory Committee for Aeronautics, 1936), by Nathan F. Scudder, H. W. Kirshbaum, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effect of free-stream Mach number on gross-force and pumping characteristics of several ejectors (National Advisory Committee for Aeronautics, 1955), by Leonard E. Stitt, Alfred S. Valerino, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Preliminary investigation of the strength and endurance of plastic-impregnated fiberglass compressor blades (National Advisory Committee for Aeronautics, 1955), by Donald F. Johnson, Andre J. Meyer, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Endurance evaluation of shell-supported turbine rotor blades made of timken 17-22A (S) steel (National Advisory Committee for Aeronautics, 1951), by Francis S. Stepka, John L. Clure, H. Robert Bear, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Preparation and properties of concentrated boron-hydrocarbon slurry fuels (National Advisory Committee for Aeronautics, 1954), by Irving A. Goodman, Virginia O. Fenn, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Effect of high pressure on smoking tendency of diffusion flames (National Advisory Committee for Aeronautics, 1954), by Glen E. McDonald, Rose L. Schalla, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Investigation of effect of notches on elevated-temperature fatigue strength of N-155 alloy (National Advisory Committee for Aeronautics, 1954), by C. A. Hoffman and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Effect of diffusion processes and temperature on smoking tendencies of laminar diffusion flames (National Advisory Committee for Aeronautics, 1953), by Rose L. Schalla, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- An analytical study of heat requirements for icing protection of radomes (National Advisory Committee for Aeronautics, 1953), by James P. Lewis, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios (National Advisory Committee for Aeronautics, 1953), by Eli Reshotko, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Photographic studies of preignition environment and flame initiation in turbojet-engine combustors (National Advisory Committee for Aeronautics, 1953), by David M. Straight, J. Dean Gernon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Effect of surface-active additives on physical behavior of 50-percent slurries of 1.5-micron magnesium in n-decane (National Advisory Committee for Aeronautics, 1955), by Murray L. Pinns, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Seven commercial organo-metallic additives (National Advisory Committee for Aeronautics, 1954), by Vincent F. Hlavin, William P. Cook, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Theory of ignition in nonturbulent and turbulent flow using long-duration discharges (National Advisory Committee for Aeronautics, 1954), by Clyde C. Swett and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Investigation of transonic turbine designed for zero diffusion of suction-surface velocity (National Advisory Committee for Aeronautics, 1954), by Warren J. Whitney, R. Y. Wong, Daniel E. Monroe, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Note on performance of aircraft ejector nozzles at high secondary flows (National Advisory Committee for Aeronautics, 1954), by Fred D. Kochendorfer, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- A summary of preliminary investigations into the characteristics of combustion screech on ducted burners (National Advisory Committee for Aeronautics, 1954), by Lewis Laboratory Staff, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Investigation of combustion screech and a method of its control (National Advisory Committee for Aeronautics, 1954), by James L. Jr Harp, Lively Bryant, Wallace W. Velie, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Investigation of acceleration characteristics of a single-spool turbojet engine (National Advisory Committee for Aeronautics, 1953), by Frank L. Oppenheimer, George J. Pack, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Free fall and evaporation of n-octane droplets in the atmosphere as applied to the jettisoning of aviation gasoline at altitude (National Advisory Committee for Aeronautics, 1953), by Herman H. Lowell, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Examination of smoke and carbon from turbojet-engine combustors (National Advisory Committee for Aeronautics, 1952), by Thomas P. Clark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Investigation of axially symmetric and two-dimensional multinozzles for producing supersonic streams (National Advisory Committee for Aeronautics, 1952), by Eli Reshotko, Rudolph C. Haefeli, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Static investigation of several jet deflectors for longitudinal control of an aircraft (National Advisory Committee for Aeronautics, 1955), by Alfred S. Valerino, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Photographic investigation of air-flow patterns in transparent one-sixth sector of annular turbojet-engine combustor with axial-slot-type air admission (National Advisory Committee for Aeronautics, 1954), by Charles C. Graves, J. Dean Gernon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Relation of turbine-engine combustion efficiency to second-order reaction kinetics and fundamental flame speed (National Advisory Committee for Aeronautics, 1954), by J. Howard Childs, Charles C. Graves, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone (National Advisory Committee for Aeronautics, 1954), by Robert R. Hibbard, Wilfred E. Scull, Allen J. Metzler, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8 (National Advisory Committee for Aeronautics, 1954), by Richard H. Cavicchi, Robert E. English, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Engine design-point performance (National Advisory Committee for Aeronautics, 1954), by James E. Hubbartt, Wilson B. Schramm, R. J. Rossbach, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging (National Advisory Committee for Aeronautics, 1954), by Wilfred E. Scull, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analytical investigation of fuel temperatures and fuel-evaporation losses encountered in long-range high-altitude supersonic flight (National Advisory Committee for Aeronautics, 1953), by Richard J. McCafferty, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Determination of surge and stall limits of an axial-flow turbojet engine for control applications (National Advisory Committee for Aeronautics, 1953), by Ross D. Schmidt, Edward W. McGraw, George Vasu, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Experimental investigation of a lightweight rocket chamber (National Advisory Committee for Aeronautics, 1953), by John E. Dalgleish, Adelbert O. Tischler, United States National Advisory Committee for Aeronautics, and Lewis Flilght Propulsion Laboratory (page images at HathiTrust)
- Variation in smoking tendency among low molecular weight hydrocarbons (National Advisory Committee for Aeronautics, 1952), by Rose L. Schalla, Glen E. McDonald, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Effect of fuel additives on carbon deposition in a J33 single combustor [Part] 1, Three metallic-organic additives (National Advisory Committee for Aeronautics, 1952), by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Investigation of effects of reynolds number on large double-entry centrifugal compressor (National Advisory Committee for Aeronautics, 1952), by Karl Kovach, Joseph R. Withee, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Influence of external variables on smoking of benzene flames (National Advisory Committee for Aeronautics, 1952), by Thomas P. Clark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Experimental investigation of free-convection heat transfer in vertical tube at large grashof numbers (National Advisory Committee for Aeronautics, 1952), by E. R. G. Eckert, A. J. Diagula, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Infiltration of titanium carbide with several metals (National Advisory Committee for Aeronautics, 1952), by Raymond S. Gurnick, Anthony L. Cooper, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Experimental cooling-air impeller performance and turbine rotor temperatures in modified J33 split-disk rotor up to speeds of 10,000 RPM (National Advisory Committee for Aeronautics, 1952), by Alfred J. Nachtigall, Robert R. Ziemer, Charles F. Zalabak, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade (National Advisory Committee for Aeronautics, 1952), by Louis J. Jr Schafer, Hadley T. Richards, Edward R. Bartoo, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Some effects of blade trailing-edge thickness on performance of a single-stage axial-flow compressor (National Advisory Committee for Aeronautics, 1951), by J. J. Moses, G. K. Serovy, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Combustion of smoke in diffusion and bunsen flames (National Advisory Committee for Aeronautics, 1951), by Thomas P. Clark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Carbon deposition of several special turbojet-engine fuels (National Advisory Committee for Aeronautics, 1951), by Jerrold D. Wear, James W. Useller, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Effects of special leading- and trailing-edge modifications on blade temperature (National Advisory Committee for Aeronautics, 1951), by Herman H. Ellerbrock, Gordon T. Smith, Charles F. Zalabak, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. [Part] 2, Isentropic-spike all-external compression inlet (National Advisory Committee for Aeronautics, 1951), by L. J. Obery, G. W. Englert, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Rotor blades with 34 steel tubes in cooling-air passages (National Advisory Committee for Aeronautics, 1950), by Robert O. Hickel, Gordon T. Smith, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air (National Advisory Committee for Aeronautics, 1950), by Eugene V. Zettle, Herman Mark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine (National Advisory Committee for Aeronautics, 1950), by William P. Cook, Richard G. Koch, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Bibliography of unclassified aircraft-fire literature (National Advisory Committee for Aeronautics, 1949), by Solomon Weiss, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (U.S.) (page images at HathiTrust; US access only)
- Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines [Part] 3, Liquid ammonia (National Advisory Committee for Aeronautics, 1952), by Vearl N. Huff, Sanford Gordon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Carbon-deposition characteristics of MIL-F-5624A fuels containing high-boiling aromatic hydrocarbons (National Advisory Committee for Aeronautics, 1952), by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Visualization of secondary-flow phenomena in blade row (National Advisory Committee for Aeronautics, 1952), by H. Z. Herzig, G. R. Costello, A. G. Hansen, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Endurance evaluation of several tube-filled rotor blades (National Advisory Committee for Aeronautics, 1952), by Jack B. Esgar, John L. Clure, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Ignition-delay characteristics in modified open-cup apparatus of several fuels with nitric acid oxidants within temperature range 70 degrees to 105 degrees F (National Advisory Committee for Aeronautics, 1951), by Riley O. Miller, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analytical investigation of two liquid cooling systems for turbine blades (National Advisory Committee for Aeronautics, 1951), by Thomas W. Jackson, John N. B. Livingood, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Diborane, pentaborane, boron, and boron-octene-1 slurries (National Advisory Committee for Aeronautics, 1951), by Benson E. Gammon and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- The use of perforated inlets for efficient supersonic diffusion (National Advisory Committee for Aeronautics, 1951), by John C. Evvard, John W. Blakey, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A summary of design information for water-cooled turbines (National Advisory Committee for Aeronautics, 1951), by John C. Freche, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Methods for connection to revolving thermocouples (National Advisory Committee for Aeronautics, 1951), by Philip R. Tarr and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Vapor-fuel-distribution effects on combustion performance of a single tubular combustor (National Advisory Committee for Aeronautics, 1950), by Richard J. McCafferty, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid (National Advisory Committee for Aeronautics, 1950), by Gerald Morrell, Jack C. Humphrey, John L. Sloop, Dezso J. Ladanyi, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Wing tip with subsonic trailing edge (National Advisory Committee for Aeronautics, 1949), by Harold Mirels, James M. Jagger, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Correlation of physical properties of ceramic materials with resistance to fracture by thermal shock (National Advisory Committee for Aeronautics, 1949), by W. G. Lidman, A. R. Bobrowsky, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Lumped reflector parameters for two-group reactor calculations (National Advisory Committee for Aeronautics, 1952), by Daniel Fieno, Robert B. Spooner, Harold Schneider, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines [Part] 2, Hydrazine (National Advisory Committee for Aeronautics, 1952), by Vearl N. Huff, Sanford Gordon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Mechanism of start and development of aircraft crash fires (National Advisory Committee for Aeronautics, 1952), by I. Irving Pinkel, Gerard J. Pesman, G. Merritt Preston, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- True airspeed measurement by ionization-tracer technique (National Advisory Committee for Aeronautics, 1952), by Bemrose Boyd, George H. Brodie, Robert G. Dorsch, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust; US access only)
- Evaluation of five conical center-body supersonic diffusers at several angles of attack (National Advisory Committee for Aeronautics, 1952), by Gerald W. Englert, Leonard J. Obery, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Blade-to-coolant heat-transfer results and operating data from a natural-convection water-cooled single-stage turbine (National Advisory Committee for Aeronautics, 1951), by Anthony J. Diaguila, John C. Freche, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Determination of blade-to-coolant heat-transfer coefficients on a forced-convection, water-cooled, single-stage turbine (National Advisory Committee for Aeronautics, 1951), by John C. Freche, Eugene F. Schum, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Conduction and film cooling of leading and trailing edges of rotor blades (National Advisory Committee for Aeronautics, 1951), by Vernon L. Arne, Jack B. Esgar, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Rotor blades with split trailing edges (National Advisory Committee for Aeronautics, 1951), by Gordon T. Smith, Robert O. Hickel, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74 (National Advisory Committee for Aeronautics, 1951), by L. Eugene Baughman, Larence I. Gould, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Determination of gas-to-blade convection heat-transfer coefficients on a forced-convection, water-cooled single-stage aluminum turbine (National Advisory Committee for Aeronautics, 1951), by John C. Freche, Eugene F. Schum, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Combustion efficiency and altitude operational limits of three liquid hydrocarbon fuels having high volumetric energy content in a J33 single combustion (National Advisory Committee for Aeronautics, 1950), by Edward G. Stricker and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Determination of aromatics and olefins in wide-boiling petroleum fractions (National Aeronautics and Space Administration, 1950), by A. E. Spakowski, R. R. Hibbard, A. Evans, United States National Advisory Committee for Aeronautics, United States National Aeronautics and Space Administration, and Lewis Flight Propulsion Laboratory (page images at HathiTrust; US access only)
- Transient operating characteristics of a turbojet engine when subjected to step changes in fuel flow (National Advisory Committee for Aeronautics, 1950), by Arthur H. Bell, J. Elmo Farmer, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Performance of supersonic axial-flow compressors based on one-dimensional analysis (National Advisory Committee for Aeronautics, 1949), by Linwood C. Wright, John F. Klapproth, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- An experimental investigation of the design variables for NACA submerged duct entrances (National Advisory Committee for Aeronautics, 1948), by Emmet A. Mossman, Lauros M. Randall, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The development of jet-engine Nacelles for a high-speed bomber design (National Advisory Committee for Aeronautics, 1947), by Robert E. Dannenberg, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane (National Advisory Committee for Aeronautics, 1951), by Richard B. Skoog, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Instrumentation of the ames supersonic free-flight wind tunnel (National Advisory Committee for Aeronautics, 1952), by Robert O. Briggs, Stanley F. Schmidt, William J. Kerwin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Downwash characteristics and vortex-sheet shape behind a 63 degree swept-back wing-fuselage combination at a Reynolds number of 6,100,000 (National Advisory Committee for Aeronautics, 1952), by William H. Tolhurst, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- An evaluation of two cooling-air ejectors in flight at transonic speeds (National Advisory Committee for Aeronautics, 1954), by L. Stewart Rolls, C. Dewey Havill, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet (National Advisory Committee for Aeronautics, 1954), by Henry A. Jr Cole, Euclid C. Holleman, Stuart C. Brown, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- The wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes (National Advisory Committee for Aeronautics, 1955), by Harvard Lomax, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Modified Wiener filter theory. (National Advisory Committee for Aeronautics, 1955), by Elwood C. Stewart, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Location of detached shock wave in front of a body moving at supersonic speeds (National Advisory Committee for Aeronautics, 1947), by Edmund V. Laitone, Otway O'M. Pardee, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Tests of a small-scale NACA submerged inlet at transonic Mach numbers (National Advisory Committee for Aeronautics, 1950), by L. Stewart Rolls, George A. Rathert, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Tests of submerged duct installation on a modified fighter airplane in the Ames forty by eighty foot wind tunnel. (National Advisory Committee for Aeronautics, 1947), by Norman J. Martin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- The effect of various missile characteristics on airframe frequency response (National Advisory Committee for Aeronautics, 1952), by Howard F. Matthews, Walter E. McNeill, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Supplementary note on modified-impact-theory calculations for bodies of revolution having minimum drag at hypersonic speeds (National Advisory Committee for Aeronautics, 1952), by Meyer M. Resnikoff, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds (National Advisory Committee for Aeronautics, 1953), by Barrett S. Baldwin, Earl D. Knechtel, John B. Turner, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations (National Advisory Committee for Aeronautics, 1955), by Jack N. Nielsen, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- A comparison at mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizonatl tail heights behind a wing with 45 degrees of sweepback (National Advisory Committee for Aeronautics, 1955), by Jack D. Stephenson, Angelo Bandettini, Ralph Selan, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane (National Advisory Committee for Aeronautics, 1947), by Emmet A. Mossman, Donald E. Gault, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability below the Mach Number of Lift Divergence (National Advisory Committee for Aeronautics, 1948), by John A. Axelson, J. Conrad Crown, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Experimental investigation of NACA submerged air inlets on a one fifth scale model of a fighter airplane. (National Advisory Committee for Aeronautics, 1947), by Donald E. Gault, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Summary of results of a wind-tunnel investigation of 9 related horiztonal tails. (National Advisory Committee for Aeronautics, 1955), by Jules B. Jr Dods, Bruce E. Tinling, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Boundary-layer measurements on several porous materials with suction applied (National Advisory Committee for Aeronautics, 1952), by George B. McCullough, Bruno J. Gambucci, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- The effects of compressibility on the upwash at the propeller planes of a four-engine tractor airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10 (National Advisory Committee for Aeronautics, 1953), by Armando E. Lopez, Jerald K. Dickson, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 (National Advisory Committee for Aeronautics, 1954), by George C. Kenyon, Robert M. Reynolds, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree swept-back wing. (National Advisory Committee for Aeronautics, 1955), by Richard S. Bray, Robert C. Innis, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- The effects of powered controls and fire-control systems on tracking accuracy (National Advisory Committee for Aeronautics, 1955), by George A. Rathert, Burnett L. Gadeberg, Marvin Abramovitz, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Correlation of heat-transfer and friction data for air flowing in inconel tube with rounded entrance (National Advisory Committee for Aeronautics, 1949), by Warren H. Lowdermilk, Milton D. Grele, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, Robert O. Jr Dietz, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Preliminary engine investigation (National Advisory Committee for Aeronautics, 1949), by Andre J. Meyer, Howard F. Calvert, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800 degrees R (National Advisory Committee for Aeronautics, 1948), by Robert C. Kohl, Robert G. Larkin, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Perforated supersonic inlet (National Advisory Committee for Aeronautics, 1948), by Albert H. Schroeder, James F. Connors, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of turbine performance and effect of tail-pipe design on engine performance (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frederick C. Foshag, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Pressure-sensitive system for gas-temperature control (National Advisory Committee for Aeronautics, 1948), by Norman Matz, Richard S. Cesaro, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Over-all engine performance (National Advisory Committee for Aeronautics, 1948), by J. C. Nettles, J. R. Easterly, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust; US access only)
- Efficiency of radial-flow turbine of turbo engineering corporation TT13-18 turbo super charger (National Advisory Committee for Aeronautics, 1947), by Earl E. Coulter, William R. Galloway, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Some methods of analyzing the effect of basic design variables on axial-flow-compressor performance (National Advisory Committee for Aeronautics, 1947), by John T. Sinnette, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Cooling of gas turbines [Part] 2, effectiveness of rim cooling of blades (National Advisory Committee for Aeronautics, 1947), by L. Wolfenstein, John S. McCarthy, Gene L. Meyer, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- Calculations of the performance of a compression-ignition engine-compressor turbine combination. [Part] 2, Performance of complete combination (National Advisory Committee for Aeronautics, 1947), by Alexander Mendelson, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- Heat transfer on an afterbody immersed in the separated wake of a hemisphere (National Advisory Committee for Aeronautics, 1958), by Helmer V. Nielsen, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), by John O. Jr Reller, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Measurement of the longitudinal moment of inertia of a flexible airplane (National Advisory Committee for Aeronautics, 1956), by Henry Ambrose Jr Cole, Frances L. Bennion, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Bemrose Boyd, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of turbine performance of 19B-8 engine (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frank L. Suozzi, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Dynamic investigation (National Advisory Committee for Aeronautics, 1949), by Andre J. Meyer, Howard F. Calvert, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Combustion-chamber performance with four fuels in bumblebee 18-inch ram jet incorporating various rake- or gutter-type flame holders (National Advisory Committee for Aeronautics, 1948), by Ephraim M. Howard, David T. Dupree, Fred A. Wilcox, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Operational characteristics (National Advisory Committee for Aeronautics, 1948), by Richard L. Golladay, Stanley L. Gendler, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Effect of fuels and fuel-nozzle characteristics on performance of an annular combustor at simulated altitude conditions (National Advisory Committee for Aeronautics, 1948), by RIchard J. McCafferty, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Ramp floor vent-tube mounting (National Advisory Committee for Aeronautics, 1948), by Robert S. Ruggeri, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- An analysis of control requirements and control parameters for direct-coupled turbojet engines (National Advisory Committee for Aeronautics, 1948), by David Novik, Edward W. Otto, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Velocity distributions on two-dimensional wing-duct inlets by conformal mapping (National Advisory Committee for Aeronautics, 1947), by W. Perl, H. E. Moses, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- Cooling of gas turbines [Part] 4, Calculated temperature distribution in the trailing part of a turbine blade using direct liquid cooling (National Advisory Committee for Aeronautics, 1947), by W. Byron Brown, William R. Monroe, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- Jet diffuser for simulating ram conditions on a turbojet-engine static test stand (National Advisory Committee for Aeronautics, 1947), by Robert H. Essig, David S. Gabriel, H. R. Bohanon, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- A transonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution (National Advisory Committee for Aeronautics, 1957), by George H. Holdaway, Elaine W. Hatfield, Minor R. Wallace, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Heat-transfer characteristics of blunt 2 and 3 dimensional bodies at supersonic speeds. (National Advisory Committee for Aeronautics, 1956), by Glen Goodwin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Development of a high-velocity free-flight launcher - the Ames light - gas gun (National Advisory Committee for Aeronautics, 1955), by A. C. Charters, Vernon J. Rossow, B. Pat Denardo, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Analysis of compressor performance (National Advisory Committee for Aeronautics, 1948), by Robert O. Dietz, John K. Kuenzig, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Operational characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Theoretical performance of diborane as a rocket fuel (National Advisory Committee for Aeronautics, 1949), by Vearl N. Huff, Virginia C. Erdmann, Clyde S. Calvert, United States National Advisory Committee for Aeronautics, and OH) Lewis Flight Propulsion Laboratory (Cleveland (page images at HathiTrust)
- Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades (National Advisory Committee for Aeronautics, 1948), by John C. Freche, Bob W. Sheflin, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Reece V. Hensley, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Natural icing of an axial-flow turboject engine in flight for a single icing condition (National Advisory Committee for Aeronautics, 1948), by Loren W. Acker, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Performance of J33 turbojet engine with shaft-power extraction [Part] 2, Compressor (National Advisory Committee for Aeronautics, 1948), by Albert O. Ross, J. Cary Nettles, J. R. Easterly, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust; US access only)
- Heat transfer from high-temperature surfaces to fluids. [Part] 1, Preliminary investigation with air in inconel tube with rounded entrance, inside diameter of 0.4 inch and length of 24 inches (National Advisory Committee for Aeronautics, 1948), by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Cooling of gas turbines [Part] 8, Theoretical temperature distributions through gas turbine with special blades and cooling fins on the rim (National Advisory Committee for Aeronautics, 1948), by W. Byron Brown, John N. B. Livingood, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Cooling of gas turbines [Part] 5, Effectiveness of air cooling of hollow blades (National Advisory Committee for Aeronautics, 1947), by L. Wolfenstein, John S. McCarthy, Robert L. Maxwell, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- Cooling of gas turbines [Part] 3, Analysis of rotor and blade temperatures in liquid-cooled gas turbines (National Advisory Committee for Aeronautics, 1947), by W. Byron Brown, John N. B. Livingood, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
- Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds (National Advisory Committee for Aeronautics, 1958), by Raymond C. Savin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring (National Advisory Committee for Aeronautics, 1957), by Fred B. Sutton, J. Walter Lautenberger, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule (National Advisory Committee for Aeronautics, 1956), by William A. Page, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- A discussion of methods for reducing aerodynamic heating in supersonic flight (National Advisory Committee for Aeronautics, 1955), by A. J. Jr Eggers, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Some recent research on the handling qualities of airplanes (National Advisory Committee for Aeronautics, 1956), by Walter C. Williams, William H. Phillips, Flight Research Center (U.S.), United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- 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), by Albert J. Evans, George Liner, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory (U.S. G.P.O., 1952), by Clarence W. Matthews and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Transverse vibrations of hollow thin-walled cylindrical beams (National Advisory Committee for Aeronautics, 1952), by Bernard Budiansky, Edwin T. Kruszewski, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Some possibilities of using gas mixtures other than air in aerodynamic research (National Advisory Committee for Aeronautics, 1954), by Dean R. Chapman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Hydrocarbon and nonhydrocarbon derivatives of cyclopropane : errata no. 1 (U.S. G.P.O., 1953), by Simon Ostrach, Louis C. Gibbons, Paul H. Wise, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- To promote the national defense by authorizing a unitary plan for the construction of transsonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center (H.R. 3434). ([U.S. G.P.O.], 1949), by United States House Committee on Armed Services, Carl Vinson, Jerome C. Hunsaker, and James Forrestal (page images at HathiTrust)
- Subcommittee hearings on H.R. 3434, to promote the national defense by authorizing a unitary plan for the construction of transonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center ([U.S. G.P.O.], 1949), by United States. Congress. House. Committee on Armed Services. Subcommittee No. 3 (page images at HathiTrust)
- Full committee hearings on H.R. 2895, S. 509, S. 1267, S. 2382, S. 2380, S. 1560, H.R. 5876 ([U.S. G.P.O.], 1949), by United States House Committee on Armed Services (page images at HathiTrust)
- Patent policies relating to aeronautical and space research : hearings before the Special Subcommittee on Patents and Scientific Inventions of the Committee on Science and Astronautics, U.S. House of Representatives, Eighty-seventh Congress, first session, on H.R. 1934 and H.R. 6030. (U.S. G.P.O., 1961), by United States House Committee on Science and Astronautics (page images at HathiTrust)
- The shearing rigidity of curved panels under compression (National Advisory Committee for Aeronautics, 1946), by Nicholas J. Hoff, Bruno A. Boley, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Properties and preparation of ceramic insulators for spark plugs (G.P.O., 1919), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Technical meetings in the flight sciences : a report to the Daniel and Florence Guggenheim Foundation. (The Company, 1959), by Pendray & Company and Daniel and Florence Guggenheim Foundation (page images at HathiTrust; US access only)
- Wing-fuselage interference tail buffeting, and air flow about the tail of a low-wing monoplane (Government Printing Office, 1934), by James A. White, Manely J. Hood, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Preignition-limited performance of several fuels (U.S. Government Printing Office, 1945), by Donald W. Male, John C. Evvard, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Comparative flutter calculations on low-aspect-ratio wings in incompressible and supersonic flows. (M.I.T. Department of Aeronautical Engineering, 1954), by Garabed Zartarian, Herbert M. Voss, and Pao Tan Hsu (page images at HathiTrust; US access only)
- Theoretical and experimental pressure distributions on low aspect ratio wings oscillating in an incompressible flow. (M.I.T. Aeroelastic and Structures Research Laboratory, 1954), by William R. Laidlaw (page images at HathiTrust; US access only)
- Material evaluation for a Mach III transport plane (Syracuse University, Metallurgical Research Laboratories, Dept. of Chemical Engineering and Metallurgy, 1961), by R. J. Sell, Volker Weiss, and Charles Trudeau Chave (page images at HathiTrust; US access only)
- Implementation plan for an air transportation research information service. (Dept. of Transportation, Federal Aviation Administration ;, 1977), by National Research Council (U.S.). Committee on Air Transportation Research Information Service and United States Federal Aviation Administration (page images at HathiTrust)
- Medical benefits from space research (National Aeronautics and Space Administration, 1968), by United States National Aeronautics and Space Administration (page images at HathiTrust)
- The near noise field of static jets and some model studies of devices for noise reduction (U.S. Government Printing Office, 1956), by Leslie W. Lassiter, Harvey H. Hubbard, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Correlation of cylinder-head temperatures and coolant heat rejections of a multicylinder, liquid-cooled engine of 1710-cubic-inch displacement (U.S. Government Printing Office, 1950), by Bruce T. Lundin, Louis J. Chelko, John H. Povolny, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Determination of vortex paths by series expansion technique with application to cruciform wings (U.S. Government Printing Office, 1957), by Alberta Y. Alksne and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA transonic wind-tunnel test sections (U.S. Government Printing Office, 1955), by Ray H. Wright, Vernon G. Ward, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The soap-bubble method of studying the combustion of mixtures of CO and O² (National Advisory Committee for Aeronautics, 1935), by Ernest F. Fiock and Carl H. Roeder (page images at HathiTrust)
- The N.A.C.A. variable-density wind tunnel (Government Printing Office, 1932), by Eastman N. Jacobs, Ira H. Abbott, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Some approximate equations for the standard atmosphere (Government Printing Office, 1931), by Walter S. Diehl and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- The influence of the form of a wooden beam on its stiffness and strength. I, Deflection of beams with special reference to shear deformations (Government Printing Office, 1923), by J. A. Newlin, G. W. Trayer, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Wind tunnel tests on airfoil boundary layer control using a backward-opening slot (National Advisory Committee for Aeronautics, 1931), by Millard J. Bamber and Langley Memorial Aeronautical Library (page images at HathiTrust)
- Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons (U.S. Government Printing Office, 1952), by William M. O'Hare, John R. Hagerman, Rodger L. Naeseth, Jack Fischel, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Structural response to discrete and continuous gusts of an airplane having wing-bending flexibility and a correlation of calculated and flight results (U.S. Government Printing Office, 1954), by John C. Houbolt, Eldon E. Kordes, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Method and graphs for the evaluation of air-induction systems (U.S. Government Printing Office, 1953), by George B. Brajnikoff and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Working charts for the determination of the lift distribution between biplane wings (Government Printing Office, 1932), by Paul Kuhn and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- General potential theory of arbitrary wing sections (Government Printing Office, 1933), by T. Theodorsen, I. E. Garrick, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Final report by the Ohio State University Research Foundation (Columbus, Oh : Ohio State University Research Foundation, 1961., 1961), by J. S. Kidd (page images at HathiTrust; US access only)
- Wind-tunnel research comparing lateral control devices particularly at high angles of attack. III : ordinary ailerons rigged up 10 ̊when neutral (Government Printing Office, 1932), by Fred E. Weick, Carl J. Wenzinger, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Tests of nacelle-propeller combinations in various positions with references to wings IV : thick wing--various radial-engine cowlings--tandem propellers. (National Advisory Committee for Aeronautics, 1934), by Theodore Theodorsen, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Library (page images at HathiTrust)
- The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders (National Advisory Committee for Aeronautics, 1934), by Oscar W. Schey, Vern G. Rollin, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Library (page images at HathiTrust)
- An investigation of the coeffecient of discharge of liquids through small round orifices (U.S. G.P.O., 1926), by W. F. Joachim and Langley Aeronautical Laboratory (page images at HathiTrust)
- Characteristics of a single float seaplane during take-off (Government Printing Office, 1925), by J. W. Crowley, K. M. Ronan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Aircraft accidents : methods of analysis (Government Printing Office, 1929), by Subdivison Special Committee on the Nomenclature and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Theories of flow similitude (Government Printing Office, 1928), by A. F. Zahm and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The aerodynamic effects of wing cut-outs (Government Printing Office, 1934), by Albert Sherman and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Characteristics of Clark Y airfoils of small aspect ratios (Government Printing Office, 1932), by C. H. Zimmerman and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- The unsteady lift of a wing of finite aspect ratio (U.S. Government Printing Office, 1940), by Robert T. Jones (page images at HathiTrust; US access only)
- Flight determination of drag of normal-shock nose inlets with various cowling profiles at mach numbers from 0.9 to 1.5 (U.S. Government Printing Office, 1956), by R. I. Sears, L. W. Putland, C. F. Merlet, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Lift hysteresis at stall as an unsteady boundary-layer phenomenon (U.S. Government Printing Office, 1956), by F. K. Moore and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence (U.S. Government Printing Office, 1957), by John M. Eggleston, Franklin W. Diederich, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Influence of hot-working conditions on high-temperature properties of a heat-resistant alloy (U.S. Government Printing Office, 1957), by John F. Ewing, J. W. Freeman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades (U.S. Government Printing Office, 1958), by Robert F. Coleman, Arnold M. Feingold, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition (U.S. Government Printing Office, 1958), by Dean R. Chapman, Howard K. Larson, Donald M. Kuehn, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds (U.S. Government Printing Office, 1957), by Percy J. Bobbitt and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Survey of hydrogen combustion properties (U.S. Government Printing Office, 1958), by Isadore L. Drell, Frank E. Belles, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A study of wing flutter (Washington, D.C. : G.P.O., 1928., 1928), by A. F. Zahm, Ernest E. Wilson, United States National Advisory Committee for Aeronautics, and United States. Navy. Bureau of Construction and Repair. Aerodynamical Laboratory (page images at HathiTrust)
- Attention value of audio and visual warning signals (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by George L. Kreezer, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Human Factors and Ergonomics Collection, and Applied Psychology Corporation (page images at HathiTrust)
- 1975 USAF/ASEE summer faculty research program : final administrative report (School of Engineering, Auburn University, 1975), by James Fred O'Brien, United States. Air Force. Office of Scientific Research, Auburn University. School of Engineering, and American Society for Engineering Education (page images at HathiTrust)
- Report of the Aeronautical Research Institute, Tōkyō Imperial University (Tōkyō Teikoku Daigaku Kōkū Kenkyūjo, 1921), by Tōkyō Teikoku Daigaku. Kōkū Kenkyūjo (page images at HathiTrust; US access only)
- Annual report including Technical reports. (U.S. Govt. Print. Off., 1915), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Pamphlet. (New York, 1926), by Daniel Guggenheim Fund for the Promotion of Aeronautics (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Donald D. Baals, Mary J. Mourhess, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
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