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Aerodynamics -- Equipment and supplies

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• Aerodynamics
• Airplanes -- Equipment and supplies
• Equipment and supplies

• Aerodynamics -- Equipment and supplies -- Design and construction
• Drag (Aerodynamics) -- Equipment and supplies
• Aerodynamics -- Measurement -- Equipment and supplies

• A smoke generator system for aerodynamic flight research (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by David M. Richwine, Gene V. Tracy, Robert E. Curry, and Dryden Flight Research Facility (page images at HathiTrust)

• Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators (National Aeronautics and Space Administration ;, 1974), by Herman L. Bohon, Robert Miserentino, James Wayne Sawyer, and Langley Research Center (page images at HathiTrust)

• Drag measurements on a laminar-flow body of revolution in the 13-inch magnetic suspension and balance system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by David A. Dress (page images at HathiTrust)

• Experimental characterization of the effects of pneumatic tubing on unsteady pressure measurements (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Stephen A. Whitmore and Dryden Flight Research Facility (page images at HathiTrust)

• Spectrographic temperature measurements in a carbon-arc-powered air jet (National Aeronautics and Space Administration, 1959), by David H. Greenshields and Langley Research Center (page images at HathiTrust)

• Flight loads measurements obtained from calibrated strain-gage bridges mounted externally on the skin of a low-aspect-ratio wing (National Aeronautics and Space Administration ;, 1976), by Clinton V. Eckstrom, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Subsonic wind-tunnel tests of a trailing-cone device for calibrating aircraft static-pressure systems (National Aeronautics and Space Administration ;, 1973), by Frank L. Jordan, Virgil S. Ritchie, and Langley Research Center (page images at HathiTrust)

• A gage and recording equipment for measuring dynamic strain in rock (U.S. Dept. of the Interior, Bureau of Mines, 1949), by Leonard Obert and Wilbur I. Duvall (page images at HathiTrust)

• Performance of a mass-flux probe in a Mach 3 stream (National Aeronautics and Space Administration ;, 1969), by Lloyd N. Krause, George E. Glawe, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)

• Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Terry J. Larson and Ames Research Center (page images at HathiTrust)

• Operational and performance characteristics of the X-15 spherical, hypersonic flow-direction sensor (National Aeronautics and Space Administration ;, 1965), by Chester H. Wolowicz, Terrence D. Gossett, and Flight Research Center (U.S.) (page images at HathiTrust)

• Experimental and analytical sonic nozzle discharge coefficients for Reynolds numbers up to 8x10⁶ (National Aeronautics and Space Administration ;, 1975), by Andrew J. Szaniszlo and Lewis Research Center (page images at HathiTrust)
• Influence of particle drag coefficient on particle motion in high-speed flow with typical laser velocimeter applications (National Aeronautics and Space Administration ;, 1976), by Michael J. Walsh and Langley Research Center (page images at HathiTrust)
• Performance of a mass-flux probe in a Mach 3 stream (National Aeronautics and Space Administration ;, 1969), by Lloyd N. Krause, George E. Glawe, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)

• Flowmeter for space (National Aeronautics and Space Administration ;, 1969), by T. F. Morris, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)

• Flight evaluation of a pneumatic system for unsteady pressure measurements using conventional sensors (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Robert E. Curry, Glenn B. Gilyard, and Dryden Flight Research Facility (page images at HathiTrust)

• Operational performance of vapor-screen systems for in-flight visualization of leading-edge vortices on the F-106B aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by John E. Lamar (page images at HathiTrust)
• Photogrammetric technique using entrained balloons for in-flight ranging of trailing vortices (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by W. L. Snow, William K. Goad, Alpheus W. Burner, and Langley Research Center (page images at HathiTrust)

• Photogrammetric technique using entrained balloons for in-flight ranging of trailing vortices (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by W. L. Snow, William K. Goad, Alpheus W. Burner, and Langley Research Center (page images at HathiTrust)

• Surface pressure measurements on a series of two-dimensional yawmeter bodies (National Aeronautics and Space Administration ;, 1976), by M. J. Goodyer, Langley Research Center, and University of Virginia. Research Laboratories for the Engineering Sciences (page images at HathiTrust)

• Evaluation of a hemispherical head flow direction sensor for inlet duct measurements (National Aeronautics and Space Administration ;, 1975), by Donald L. Bennett and Flight Research Center (U.S.) (page images at HathiTrust)

• Evaluation of electrolytic tilt sensors for measuring model angle of attack in wind tunnel tests (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Douglas T. Wong and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Abriss der Strömungslehre (second edition, in German; Gottingen: Gottingen University Press, 2017), by Ludwig Prandtl (PDF at Gottingen University Press)
• Aerodynamic Design Guidelines and Computer Program for Estimation of Subsonic Wind Tunnel Performance (Washington: NASA, 1976), by William T. Eckert and Kenneth W. Mort (page images at HathiTrust)
• Airplane Aerodynamics (third edition; New York et al.: Pitman Pub. Corp., 1961), by Daniel O. Dommasch, Sydney S. Sherby, and Thomas F. Connolly (page images at HathiTrust)
• Wind Tunnel Investigation of the Interaction and Breakdown Characteristics of Slender-Wing Vortices at Subsonic, Transonic, and Supersonic Speeds (NASA Technical Paper 3114; 1991), by Gary E. Erickson (page images at HathiTrust)
• Elements of Practical Aerodynamics (New York: J. Wiley and Sons; London: Chapman and Hall, 1936), by Bradley Jones (page images at HathiTrust)
• Engineering Aerodynamics (New York: Ronald Press Co., c1928), by Walter S. Diehl (page images at HathiTrust)
• Natural Aerodynamics (New York et al.: Pergamon Press, c1958), by R. S. Scorer (page images at HathiTrust)
• Introduction to the Aerodynamics of Flight, by Theodore A. Talay (illustrated HTML at NASA)
• Aerodynamics of a Tilting Ducted Fan Configuration (NASA Technical note D-785; Washington: National Aeronautics and Space Administration, 1961), by Paul F. Yaggy and Kenneth W. Goodson (page images at HathiTrust)
• Bulletin de l'Institut aérodynamique de Koutchino. (Impr. I.N. Kouchnéreff 8 c-ie [etc.], 1909), by Russia. Institut Aėrodinamicheski ̌institut Kuchino and Dmitriĭ P. Ri͡abushinskiĭ (page images at HathiTrust; US access only)
• Original solutions of several problems in aerodynamics. (Tuttle, Morehouse & Taylor, printers, 1882), by Eli W. Blake (page images at HathiTrust)
• The analytical development of curves and streamline shapes. (Deemar Co., 1948), by Harry Hermann Haase (page images at HathiTrust)
• Abriss der Lehre von der Flüssigkeits- und Gasbewegung (G. Fischer, 1913), by Ludwig Prandtl (page images at HathiTrust; US access only)
• Mathematical theory of compressible fluid flow (Academic Press, 1958), by Richard Von Mises (page images at HathiTrust)
• Hydrodynamique générale; fluides parfaits et visqueux. Ailes d'avion. (Delagrave, 1928), by H. Bouasse (page images at HathiTrust; US access only)
• Führer durch die strömungslehre (J.W. Edwards, 1947), by Ludwig Prandtl (page images at HathiTrust)
• Fluid dynamics and applications (College of Engineering, New York University, 1941), by K. O. Friedrichs and New York University. College of Engineering (page images at HathiTrust)
• Theorie des Widerstandes der Luft bei der Bewegung der Körper ... (Vandenhoeck und Ruprecht, 1831), by Johann Karl Eduard Schmidt (page images at HathiTrust)
• Aerodynamics of the psychrometer (University of Delaware, 1926), by George Porter Paine (page images at HathiTrust)
• Vier Abhandlungen zur Hydrodynamik und Aerodynamik (Flüssigkeit mit kleiner Reibung; Traflügeltheorie, I. und II. Mitteilung; Schraubenpropeller mit geringstem Enegrieverlust) (Selbstverlag des Kaiser Wilhelm-Instituts für Strömungsforschung, 1927), by L. Prandtl and Albert Betz (page images at HathiTrust; US access only)
• Théorie des surgaces portantes; la théorie de Prandtl (Gauthier-Villars et cie, 1923), by Maurice Roy (page images at HathiTrust; US access only)
• Report ACA. ([Melbourne.], 1944), by Australia. Department of Supply. Aeronautical Research Consultative Committee (page images at HathiTrust)
• Methods of linearization in compressible flow. (Headquarters, Air Matériel Command, Wright Field, 1948), by Francis Edward Ehlers, United States. Army Air Forces. Matériel Command, and Brown University. Graduate School (page images at HathiTrust)
• Selected topics in fluid mechanics, Summer session 1946 [New York University?] ([New York?], 1946), by K. O. Friedrichs (page images at HathiTrust)
• NIR-TM V. (Amsterdam., in the 20th century), by Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands) (page images at HathiTrust; US access only)
• Étude sur l'aviation (C. Béranger, 1909), by Maurice de Cantelou (page images at HathiTrust; US access only)
• L'aviation (F. Alcan, 1913), by Paul Painlevé, Charles Maurain, and Emile Borel (page images at HathiTrust; US access only)
• Flugtechnik; Grundlagen des Kunstfluges (R. Oldenbourg, 1919), by Arthur Pröll (page images at HathiTrust; US access only)
• Fliegerkraftlehre (S. Hirzel, 1920), by Otto Heinrich Wiener (page images at HathiTrust; US access only)
• La résistance de l'air; examen des formules et des expériences (H. Dunod et E. Pinat, 1910), by Gustave Eiffel (page images at HathiTrust; US access only)
• La résistance de l'air et le vol des oiseaux (Gauthier-Villars, 1911), by Maurice Gandillot (page images at HathiTrust; US access only)
• Grundlagen der Flugtechnik; entwerfen und berechnen von Flugzeugen (B.G. Teubner, 1920), by H. G. Bader (page images at HathiTrust; US access only)
• 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)
• Aérodonétique (Gauthier-Villars et cie, 1916), by F. W. Lanchester and C. Benoit (page images at HathiTrust; US access only)
• L'aviation actuelle (F. Alcan, 1928), by A. Toussaint (page images at HathiTrust; US access only)
• Bases théoriques de l'aéronautique. (Gauthier-Villars et cie, 1916), by Nikolaĭ Egorovich Zhukovskiĭ and S. Drzewiecki (page images at HathiTrust; US access only)
• Die mechanischen grundgesetze der flugtechnik unter der vereinfachenden annahme konstanten spezifischen volumens der atmosphärischen luft. (Selbstverlag des verfassers, kommissionsverlag von Lehmann & Wentzel, 1904), by Arthur Budau (page images at HathiTrust; US access only)
• Beiträge zur Theorie des Segelns auf Grund der neueren durch Versuche und Erfahrungen der Luftfahrt gewonenen aerodynamischen Erkenntnisse über die Strömungsvorgänge an Flächen (J. Springer, 1925), by H. Croseck (page images at HathiTrust; US access only)
• Die hydrodynamischen grundlagen des fluges (F. Vieweg & sohn, 1917), by R. Grammel and Fritz Emde (page images at HathiTrust; US access only)
• Les lois expérimentales de l'aviation (Librairie aéronautique, 1911), by Alexandre Sée (page images at HathiTrust; US access only)
• Leitfaden der Flugtechnik. (J. Springer, 1913), by Siegmund Huppert (page images at HathiTrust; US access only)
• Causeries techniques sans formules sur l'aéroplane. (Librairie aéronautique, 1913), by Émile Auguste Duchêne (page images at HathiTrust; US access only)
• Design data for aeronautics and astronautics; a compilation of existing data. (Wiley, 1962), by Richard Boyd Morrison (page images at HathiTrust)
• Mécanique de l'aviation; application des méthodes de la mécanique rationnnelle à l'étude du vol et de la construction des avions. (Gauthier-Villars et cie, 1925), by Antoine Charles Alayrac (page images at HathiTrust; US access only)
• Der schwebflug und die fallbewegung ebener tafeln in der luft. (L. Friederichsen & co., 1897), by Friedrich Ahlborn (page images at HathiTrust)
• The aerodynamics of powered flight. (Wiley, 1960), by Robert Leon Carroll (page images at HathiTrust)
• Aerodynamics of the aeroplane (The Ronald press company, 1944), by W. L. Cowley (page images at HathiTrust)
• Aeronautics in theory and experiment (E. Arnold, 1920), by W. L. Cowley and H. Levy (page images at HathiTrust; US access only)
• Airplane aerodynamics (Pitman Pub. Corp., 1951), by Daniel O. Dommasch (page images at HathiTrust)
• Flight with out formulæ. (Longmans, Green and co., 1916), by Emile Duchêne and John H. Ledeboer (page images at HathiTrust; US access only)
• Sustentation, propulsion, évolution de l'aéroplane. (Librairie aéronautique, 1910), by Henri Dujardin (page images at HathiTrust; US access only)
• Recherches expérimentales sur la résistance de l'air exécutées à la tour Eiffel (Librairie aéronautique, 1909), by Gustave Eiffel (page images at HathiTrust; US access only)
• The resistance of the air and aviation experiments conducted at the Champ-de-Mars laboratory (Constable & company ltd.; Boston and New York, Houghton Mifflin company, 1913), by Gustave Eiffel and Jerome Clarke Hunsaker (page images at HathiTrust; US access only)
• Aerodynamics, : constituting the first volume of a complete work on aerial flight, (A. Constable, 1907), by F. W. Lanchester (page images at HathiTrust)
• Aerodonetics : constituting the second volume of a complete work on aerial flight (A. Constable, 1908), by F. W. Lanchester (page images at HathiTrust)
• Experimental aerodynamics (Pitman publishing corporation, 1940), by Henry Christensen Pavian and Phillip Lincoln Michel (page images at HathiTrust)
• Théorie des hélices propulsives marines et aériennes et des avions en vol rectiligne (Gauthier-Villars et cie, 1920), by Auguste Rateau (page images at HathiTrust; US access only)
• Applied wing theory (McGraw-Hill book company, inc., 1932), by Elliott Gray Reid (page images at HathiTrust; US access only)
• Aerodynamics (McGraw-Hill, 1946), by A. Wiley Sherwood (page images at HathiTrust; US access only)
• Théorie du vol des avions (É. Chiron, 1920), by Rodolphe Soreau (page images at HathiTrust; US access only)
• Dynamics of airplanes and airplane structures (J. Wiley, 1931), by John E. Younger and Baldwin Munger Woods (page images at HathiTrust)
• Smoke streams : visualized air flow (Coward-McCann, 1943), by Charles Townsend Ludington (page images at HathiTrust)
• Isoperimetrische aufgaben aus der theorie des fluges ... (Dieterichsche universitäts-buckdruckerei, 1919), by Max M. Munk (page images at HathiTrust; US access only)
• Fundamentals of fluid dynamics for aircraft designers (The Ronald press company, 1929), by Max M. Munk (page images at HathiTrust)
• Mathematics of flight (McGraw-Hill book company, inc., 1943), by James Naidich (page images at HathiTrust; US access only)
• High-speed aerodynamics. (Prentice-Hall, 1948), by Harold Ward Sibert (page images at HathiTrust)
• The mechanical principles of the aeroplane (J. & A. Churchill, 1921), by Selig Brodetsky (page images at HathiTrust; US access only)
• Simple aerodynamics and the airplane. (U. S. Govt. print. off., 1927), by United States. Army. Air Corps and Charles Norton Monteith (page images at HathiTrust)
• Simple aerodynamics and the airplane (The Ronald press company, 1929), by Clifton Carroll Carter and Charles Norton Monteith (page images at HathiTrust)
• Simple aerodynamics and the airplane (The Ronald Press Company, 1940), by Clifton Carroll Carter (page images at HathiTrust)
• Aerodynamics for model airplanes; how and why a model airplane flies (A. S. Barnes, 1952), by Donald K. Foote (page images at HathiTrust)
• L'aéroplane étudié et calculé par les mathématiques élémentaires. (R. Chapelot & cie, 1910), by Émile Auguste Duchêne (page images at HathiTrust; US access only)
• Computation curves for compressible fluid problems (J. Wiley, 1949), by Charles Lee Dailey and Frances Caldwell Wood (page images at HathiTrust)
• The measurement of fluid velocity and pressure (E. Arnold & co., 1924), by John Robert Pannell and Robert Alexander Frazer (page images at HathiTrust; US access only)
• The mechanics of the aeroplane : a study of the principles of flight. (Longmans, Green and co., 1912), by Emile Duchêne, T. O'B. Hubbard, and John H. Ledeboer (page images at HathiTrust; US access only)
• Principles of aerodynamics (McGraw-Hill, 1949), by James H. Dwinnell (page images at HathiTrust)
• Modern flight dynamics. (Prentice-Hall, 1961), by W. Richard Kolk (page images at HathiTrust)
• Introduction to aeronautical dynamics. (Wiley, 1953), by Manfred Rauscher (page images at HathiTrust)
• L'aviation; conferences faites en 1909 à la Société d'encouragement pour l'industrie nationale. (H, Dunod et E. Pinat, 1909), by Paul Renard (page images at HathiTrust; US access only)
• Basic wing and airfoil theory. (McGraw-Hill, 1951), by Alan Pope (page images at HathiTrust)
• Aeroplane designing for amateurs (Reilly & Britton, 1912), by Victor Lougheed (page images at HathiTrust)
• Basic fluid mechanics. (McGraw-Hill, 1963), by J. Lister Robinson (page images at HathiTrust)
• Lois mathématiques de la résistance des fluides. Théorie de l'hélice (O. Doin, 1921), by Henri Louis Émile Willotte (page images at HathiTrust; US access only)
• Vorträge aus dem gebiete der hydro- und aerodynamik (Innsbruck 1922) (J. Springer, 1924), by Theodore Von Kármán and Tullio Levi-Civita (page images at HathiTrust; US access only)
• L'aviation (F. Alcan, 1911), by Paul Painlevé and Emile Borel (page images at HathiTrust; US access only)
• L'aviation (F. Alcan, 1911), by Paul Painlevé and Emile Borel (page images at HathiTrust; US access only)
• Die windkraft in theorie und praxis, gemeinverständliche aerodynamik. (P. Parey, 1927), by Kurt Bilau (page images at HathiTrust; US access only)
• Principles of aerodynamics. (Pitman Pub. Corp., 1953), by Daniel O. Dommasch (page images at HathiTrust)
• Airplane aerodynamics (Pitman Pub. Corp., 1957), by Daniel O. Dommasch (page images at HathiTrust; US access only)
• La résistance de l'air et l'aviation; expériences effectuées au Laboratoire du Champ-de-Mars (H. Dunod et E. Pinat, 1910), by Gustave Eiffel (page images at HathiTrust; US access only)
• Simplified theory of flight (D. Van Nostrand company, inc., 1941), by Thomas Charles Gillmer and Herman Erich Nietsch (page images at HathiTrust)
• Essai d'aérodynamique du plan. (Hachette et cie, 1911), by Armand Antoine Agʾenor de Gramont (page images at HathiTrust; US access only)
• Homogénéité et similitude en aérodynamique. (Ė. Chiron, 1928), by Albert Métral (page images at HathiTrust; US access only)
• Les secrets du vol; les aéroplanes stabilisés; la sécurité dans le vol (Morice fréres, imprimeurs, 1928), by D Nault (page images at HathiTrust; US access only)
• Technical aerodynamics. (Distributed by Ulrich's Book Store, 1955), by Karl Dawson Wood (page images at HathiTrust)
• Über die wirkungsweise zylindrischer sonden zur untersuchung aërodynamischer felder ... (Buchdruckerei E. Birkhäuser & cie., 1920), by Fritz Ebi (page images at HathiTrust; US access only)
• Die verwendung des Wellenkampschen schleppsystems für aerodynamische untersuchungen ... (Druck von C. Donath, 1914), by Albert Sommer (page images at HathiTrust; US access only)
• Notes on dynamics for aerodynamicists. (Santa Monica, Calif., 1951), by Julius David Schetzer and inc. Douglas Aircraft Company (page images at HathiTrust)
• The theory and performance of axial-flow fans (McGraw-Hill Book Co., 1937), by Curt Keller, John Robert Weske, and Lionel S. Marks (page images at HathiTrust; US access only)
• Sailing aerodynamics. (Philosophical Library, 1954), by John Morwood (page images at HathiTrust)
• Theorie und Praxis der Flugtechnik (R.C. Schmidt, 1911), by Paul Painlevé, A. Schöning, and Emile Borel (page images at HathiTrust; US access only)
• Aerodynamik (R. C. Schmidt & co., 1922), by Richard Fuchs and Ludwig Hopf (page images at HathiTrust; US access only)
• Spanwise air-load distribution. War Department, Air Corps. Navy Department, Bureau of Aeromautics. Department of Commerce, Bureau of Air Commerce. (U.S. Govt. Print. Off., 1938), by United States. Army-Navy-Commerce Committee on Aircraft Requirements (page images at HathiTrust)
• Aircraft design data ... (Govt. print. off., 1919), by United States. Navy Department. Bureau of Construction and Repair (page images at HathiTrust)
• Die gesetze des gleichgewichts und der bewegung flüssiger körper. (S.L. Crusius, 1806), by Leonhard Euler and H. W. Brandes (page images at HathiTrust)
• Report on wind tunnel test of electric railway cars for the Philadelphia & Western Railway Company and the Cincinnati & Lake Erie Railroad Company. (Ann Arbor, 1931), by Felix Wladyslaw Pawlowski, Cincinnati and Lake Erie Railroad Company, and Philadelphia and Western Railway Company (page images at HathiTrust)
• Festigkeitslehre und Materialkunde für das Flugwesen. Teil 1 (C.J.E. Volckmann, 1917), by Hans Pietzsch (page images at HathiTrust; US access only)
• Théorie géométrique et mécanique de l'hélice-turbine. Expériences sur la résistance de l'air. (Librairie aéronautique, 1910), by Louis Marie Le Dantec (page images at HathiTrust; US access only)
• Research memorandum. (National Advisory Committee for Aeronautics, in the 20th century), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The wind and beyond : a documentary journey into the history of aerodynamics in America (Washington, D.C. : National Aeronautics and Space Administration, NASA History Office, Office of External Relations, 2003-<2007>, 2003), by James R. Hansen (page images at HathiTrust)
• NASA TR (National Aeronautics and Space Administration :, 1959), by United States National Aeronautics and Space Administration (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)
• Note on the calculation of boundary layers (National Advisory Commitee for Aeronautics, 1940), by Ludwig Prandtl and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Elementary laboratory aerodynamics (The Ronald press company, 1929), by Arthur L. Jordan (page images at HathiTrust)
• Graphische Berechnungs-Methoden : im Dienste der Naturwissenschaft und Technik (Verlag Gebr. Leemann, 1910), by Hans Mettler (page images at HathiTrust; US access only)
• Einführung in die mechanik, mit einfachen beispielen aus der flugtechnik (J. Springer, 1917), by Th. Pöschl (page images at HathiTrust; US access only)
• Aufgaben aus der technischen Mechanik. (J. Springer, 1907), by Ferdinand Wittenbauer (page images at HathiTrust; US access only)
• Applied aerodynamics (Longmans, Green and Co., 1920), by Leonard Bairstow (page images at HathiTrust; US access only)
• Aerodyamics of the helicopter (Macmillan, 1952), by Alfred Gessow (page images at HathiTrust)
• Aérodynamique (Gauthier-Villars et Cie., 1916), by N. Joukowski and S. Drzewiecki (page images at HathiTrust; US access only)
• Einführung in die Aeronautik. I. Teil. Theoretische Grundlagen; elementare Vorträge (Veit & comp., 1911), by Adolf Lippmann (page images at HathiTrust; US access only)
• Simple aerodynamics and the airplane (The Ronald Press company, 1929), by Charles Norton Monteith, Clifton Carroll Carter, and Edwin Eugene Aldrin (page images at HathiTrust)
• Airplane design; performance. (McGraw-Hill, 1936), by Edward Pearson Warner (page images at HathiTrust; US access only)
• Aerodynamics of the propeller (Air Documents Division, Intelligence Dept., Air Material Command, 1948), by Fritz Weinig (page images at HathiTrust)
• The elements of aerofoil and airscrew theory (The University Press, 1926), by H. Glauert (page images at HathiTrust)
• Resistance of air and the question of flying. Experimental lecture read by Arnold Samuelson ... (Boysen & Maasch;, 1905), by Arnold Samuelson (page images at HathiTrust; US access only)
• Studies on dynamics and instrumentation of the Holloman track (Holloman Air Force Base, New Mexico : Air Force Missile Development Center, Air Research and Development Command, 1959., 1959), by Air Force Missile Development Center (U.S.) and Knox Millsaps (page images at HathiTrust)
• Flight control system manuals. (The Division], 1952), by Inc. Northrop Aircraft and United States. Navy Dept. Bureau of Aeronautics (page images at HathiTrust)
• On the two-dimensional flow of air past a series of Rankine ovals (Catholic University of America, 1932), by Laurence Ward Sheridan (page images at HathiTrust; US access only)
• L'air et la vitesse; vues nouvelles sur l'aviation (Librairie aéronautique, 1919), by René Lorin (page images at HathiTrust; US access only)
• Practical aerodynamics and the theory of the aeroplane. A résumé of the principles evolved by past experiments. (Aeronautics Office, 1909), by Baden Fletcher Smyth Baden-Powell (page images at HathiTrust)
• Aeronautics in theory and experiment (E. Arnold, 1918), by William Lewis Cowley and H. Levy (page images at HathiTrust; US access only)
• The laws of Avanzini : laws of planes moving at an angle in air and water (E. & F.N. Spon ;, 1912), by Richard De Villamil and Giugeppe Avanzini (page images at HathiTrust)
• Simple aerodynamics and the airplane. (McCook Field, 1925), by United States. Army. Air Corps and Charles Norton Monteith (page images at HathiTrust; US access only)
• Vier Abhandlungen zur Hydrodynamik und Aerodynamik (Flüssigkeit mit kleiner Reibung; Tragflügeltheorie, I. und II. Mitteilung; Schraubenpropeller mit geringstem Energieverlust) (Selbstverlag des Kaiser Wilhelm-Instituts für Strömungsforschung, 1943), by Ludwig Prandtl and Albert Betz (page images at HathiTrust; US access only)
• Caratteristiche aerodinamiche di ali. (Tipografia Befani, 1925), by Italy. Direzione generale del genio aeronautico (page images at HathiTrust; US access only)
• Aerodynamics (The Macmillan Company, 1944), by Leslie Rendall Parkinson (page images at HathiTrust)
• Flight without formulae; simple discussions on the mechanics of the aeroplane (Longmans, Green and co., 1916), by Émile Auguste Duchêne and John Henry Ledeboer (page images at HathiTrust; US access only)
• Airplane design; aerodynamics. (McGraw-Hill book company, inc., 1927), by Edward Pearson Warner (page images at HathiTrust)
• Aerodynamics : constituting the first volume of a complete work on aerial flight, with appendices on the velocity and momentum of sound waves, on the theory of soaring flight, etc. (Constable, 1918), by F. W. Lanchester (page images at HathiTrust)
• La photographie du vent : etude photographique du champ aérodynamique. (Gauthier-Villars, 1911), by Auguste Lafay (page images at HathiTrust; US access only)
• The mechanics of the aeroplane; a study of the principles of flight (Longmans, Green and Co., 1915), by Émile August Duchêne, Thomas O'Brien Hubbard, and John Henry Ledeboer (page images at HathiTrust; US access only)
• Essais sur la résistance de l'air et le calcul des aéroplanes (Impr. A. Anselme, 1911), by Joseph Chovet (page images at HathiTrust; US access only)
• Über messung von dynamischem und statischen druck bewegter luft. (R. Oldenbourg, 1904), by Otto Krell (page images at HathiTrust; US access only)
• Über die Lage des aerodynamischen Druckmittelpunktes an ebenen und gewölbten Flächen ... (Druck von Lüdtke & Martens, 1912), by Rudolf Benitt (page images at HathiTrust; US access only)
• Technical note BN. (College Park., in the 1950s), by College Park. Institute for Fluid Dynamics and Applied Mathematics University of Maryland (page images at HathiTrust; US access only)
• Thermal effects on static aeroelastic stability and control. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1959), by Bell Aircraft Corp (page images at HathiTrust)
• Aircraft aerodynamics (Aerodinamika samoleta) Translation. (Distributed by United States Department of Commerce, Office of Technical Services, 1959), by I. V. Ostoslavskiĭ (page images at HathiTrust)
• Recirculation principle for ground effect machine two-dimensional tests. (Obtainable from Armed Services Technical Information Agency], 1962), by Orlando Martin Company. Aerospace Division (page images at HathiTrust)
• Validity of air data equations at high altitudes. (Buffalo, 1960), by Cornell Aeronautical Laboratory (page images at HathiTrust)
• The turbulent boundary layer with variable Prandtl number. (Downey, Calif., 1954), by inc North American Aviation and E. R. Van Driest (page images at HathiTrust)
• An analytical and experimental study of the ionized flow field about a hemisphere cylinder and its effect on the radiation pattern of a slot antenna (U. S. Dept. of Commerce, Office of Technical Services], 1963), by James T. Curtis, R. A. Hayman, A. F. Burke, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Aerodynamics of deflected slipstreams. (Cornell Aeronautical Laboratory, 1961), by Alexander Sowyrda (page images at HathiTrust; US access only)
• Theoretical investigation of ducted propeller aerodynamics (Republic Aviation, 1960), by Theodore Theodorsen (page images at HathiTrust)
• Stability of the boundary layer (Air Material Command, Wright-Patterson Air Force Base, 1948), by Peter Chiarulli and John Clinton Freeman (page images at HathiTrust)
• La mécanique de l'aviation (Librairie aéronautique, 1917), by René Devillers (page images at HathiTrust; US access only)
• Theoretical and experimental studies of airfoil characteristics in nonuniform sheared flow. (U. S. Army Aviation Materiel Laboratories], 1965), by William Gordon Brady (page images at HathiTrust)
• Laminar boundary layers on moving walls. ([Ithaca, N.Y.], 1956), by Stanley Harold Smith (page images at HathiTrust; US access only)
• The aerodynamic appraisal of STOL/VTOL configurations (Cornell Aeronautical Laboratory, 1960), by Robert J. Vidal, Richard A. Hartunian, and A. Sowyrda (page images at HathiTrust)
• Theoretical aerodynamics. (Ithaca, N.Y., 1951), by William Rees Sears (page images at HathiTrust)
• Applied aerodynamics (Longmans, Green and co., 1920), by Leonard Bairstow (page images at HathiTrust; US access only)
• Air forces on circular cylinders, axes normal to the wind, with special reference to dynamical similarity (U.S. Dept. of Commerce, Bureau of Standards :, 1920), by Hugh L. Dryden and United States. National Bureau of Standards (page images at HathiTrust)
• The unsteady flow field about a right circular cone in unsteady flight. (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1967), by E. A. Brong, Ohio. Research and Technology Division Air Force Flight Dynamics Laboratory (U.S.) Wright-Patterson Air Force Base, and General Electric Company. Reentry Systems Department (page images at HathiTrust)
• Mathematical aspects of subsonic and transonic gas dynamics. (Wiley, 1958), by Lipman Bers (page images at HathiTrust)
• Introduction to aerodynamics of a compressible fluid (Wiley, 1948), by H. W. Liepmann and Allen E. Puckett (page images at HathiTrust)
• Der Flug : ein auf der Wirkung strahlenden Luftdrucks beruhender Vorgang (Jung & Co., 1908), by Emil Jacob (page images at HathiTrust; US access only)
• Prinzipien der Flugtechnik (C.J.E. Volckmann nachfolger (E. Wette), 1910), by Aladár Zsélyi (page images at HathiTrust; US access only)
• Aerodynamics for pilots (U.S. Govt. print. off., 1940), by Bradley Jones (page images at HathiTrust; US access only)
• Physics of aerodynamic noise. (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), by A. V. Rimskiĭ-Korsakov (page images at HathiTrust; US access only)
• Aerodynamics/ACEE (National Aeronautics and Space Administration :, 1981), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aeronautical facilities catalogue (Washington, D.C. : Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985, 1985), by Frank E. Peñaranda, M. Shannon Freda, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight dynamics in moving air (National Aeronautics and Space Administration ;, 1971), by I︠U︡riĭ Pavlovich Dobrolenskiĭ (page images at HathiTrust; US access only)
• Low speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Dana Morris Dunham and Langley Research Center (page images at HathiTrust)
• Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by David E. Reubush, Bobby L. Berrier, and Langley Research Center (page images at HathiTrust)
• Influence of wind shear on the aerodynamic characteristics of airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1988), by Dan D. Vicroy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Harry W. Carlson, Christine M. Darden, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Weak-wave analysis of shock interaction with a slipstream (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• On the nonlinear three-dimensional instability of Stokes layers and other shear layers to pairs of oblique waves (National Aeronautics and Space Administration ;, 1992), by Xuesong Wu, Stephen J. Cowley, Sang Soo Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Detailed flow-field measurements over a 75 ̊swept delta wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Scott O. Kjelgaard, William L. Sellers, and Langley Research Center (page images at HathiTrust)
• Flow-induced resonance of screen-covered cavities (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Paul T. Soderman and Ames Research Center (page images at HathiTrust)
• Natural laminar flow experiments on modern airplane surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Bruce J. Holmes, Long P. Yip, Clifford J. Obara, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aeroacoustic and aerodynamic applications of the theory of nonequilibrium thermodynamics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by W. Clifton Horne, Krishnamurty Karamcheti, Charles A. Smith, and Ames Research Center (page images at HathiTrust)
• Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Gary E. Erickson and Langley Research Center (page images at HathiTrust)
• Ground effects on the low-speed aerodynamics of a powered, generic hypersonic configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Gregory M. Gatlin and Langley Research Center (page images at HathiTrust)
• Numerical study of the aerodynamic effects of using sulfur hexafluoride as a test gas in wind tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by W. Kyle Anderson and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface (National Aeronautics and Space Administration, 1959), by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Grid generation and flow solution method for Euler equations on unstructured grids (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by W. Kyle Anderson and Langley Research Center (page images at HathiTrust)
• Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by John W. Paulson, James L. Thomas, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic properties of a flat plate with cavity for optical-propagation studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Donald A. Buell, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Jim A. Penland, James B. Hallissy, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Blair B. Gloss, Karen E. Washburn, Edward J. Ray, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Prediction method for two-dimensional aerodynamic losses of cooled vanes using integral boundary-layer parameters (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Louis J. Goldman, Raymond E. Gaugler, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Investigation of the asymmetric aerodynamic characteristics of cylindrical bodies of revolution with variations in nose geometry and rotational orientation at angles of attack to 58ånd Mach numbers to 2 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Robert L. Kruse, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Milton Lamb and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Wind-tunnel investigation of an armed mini remotely piloted vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Arthur E. Phelps, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Parametric study of a canard-configured trasport using conceptual design optimization (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1985), by P. Douglas Arbuckle, Steven M. Sliwa, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Downwash in the plane of symmetry of an elliptically loaded wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by James D. Phillips and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream mach numbers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Mary L. Mason, Lawrence E. Putnam, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by J. P. Mendoza and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Secondary electron emission characteristics of ion-textured copper and high-purity isotropic graphite surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Arthur N. Curren, Kenneth A. Jensen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A spatial model of wind shear and turbulence for flight simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by C. Warren Campbell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by John C. Lin, R. Balasubramanian, Michael J. Walsh, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Microstructure and orientation effects on properties of discontinuous silicon carbide/aluminum composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by David L. McDanels, Charles A. Hoffman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by Mary L. Mason, Richard J. Re, Lawrence E. Putnam, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Harry W. Carlson, Christine M. Darden, and Langley Research Center (page images at HathiTrust)
• Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Rodney O. Bailey, Jack J. Brownson, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Environmental effects on space shuttle reusable surface insulation coated with reaction cured glass (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Philip O. Ransone, John E. Minster, J. D. Morrison, Langley Research Center, John F. Kennedy Space Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Charles J. Trefny, Joseph W. Wasserbauer, and Lewis Research Center (page images at HathiTrust)
• Longitudinal aerodynamic characteristics at Mach Numbers from 1.60 to 2.86 for a spanmissile with three wing planforms (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by M. Leroy Spearman, Wallace C. Sawyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers (National Aeronautics and Space Administration, 1986), by John C. Wilson, Henry L. Kelley, United States. Army Aviation Research and Technology Activity. Aerostructures Directorate, Langley Research Center, United States. Army Aviation Systems Command, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A simple method for converting frequency-domain aerodynamics to the time domain (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by E. H. Dowell and Langley Research Center (page images at HathiTrust)
• Passive control of wing/store flutter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Wilmer H. Reed, Jerome T. Foughner, F. W. Cazier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William P. Henderson, William Kelly Abeyounis, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Gregory D. Riebe, Jimmy L. Pittman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by James M. Luckring, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by P. Frank Quinto, John W. Paulson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Buffet characteristics of the F-8 supercritical wing airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by V. Michael DeAngelis, Richard C. Monaghan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• The compressible aerodynamics of rotating blades based on an acoustic formulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Lyle N. Long and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flow through very porous screens (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Paul A. Durbin, Kenneth Kenichiro Muramoto, and Lewis Research Center (page images at HathiTrust)
• A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Milton Lamb, Charles D. Trescot, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effects of conventional and square stores on the longitudinal aerodynamic characteristics of a fighter aircraft model at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by William J. Monta, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Design and performance of a high-pressure-ratio, highly loaded axial-flow transonic compressor space (National Aeronautics and Space Administration ;, 1974), by George W. Lewis, Edward R. Tysl, Lonnie Reid, and Lewis Research Center (page images at HathiTrust)
• Experimental aerodynamic characteristics for a cylindrical body of revolution with various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 (National Aeronautics and Space Administration ;, 1974), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
• Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 (National Aeronautics and Space Administration ;, 1975), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
• Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 (National Aeronautics and Space Administration ;, 1975), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
• Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Walter A. Vahl, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Elastic deformation effects on aerodynamic characteristics for a high-aspect-ratio supercritical-wing model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by Judith J. Watson and Langley Research Center (page images at HathiTrust)
• Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Zachary T. Applin, Garl L. Gentry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil (National Aeronautics and Space Administration ;, 1975), by William D. Beasley, William D. McGhee, and Langley Research Center (page images at HathiTrust)
• Flow-separation patterns on symmetric forebodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Earl R. Keener (page images at HathiTrust)
• Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Emma Jean Landrum, C. Donald Babb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• NASA Aerodynamics Program : annual report 1990 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Louis J. Williams and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Performance of low-pressure-ratio low-tip-speed fan stage with blade tip solidity of 0.65 (National Aeronautics and Space Administration ;, 1976), by George Kovich, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)
• Influence of surface static-pressure orifices on boundary-layer transition (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982), by Dan M. Somers, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by A. B. Blair, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Performance with and with inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James F. Schmidt, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by George H. Neiner, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Long P. Yip, John W. Paulson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Improvement of maneuver aerodynamics by spanwise blowing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Gary E. Erickson and James F. Campbell (page images at HathiTrust)
• Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : II-performance with coolant flow ejection at temperature ratios up to 2 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Jeffrey E. Haas, Milton G. Kofskey, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Water-tunnel investigation of concepts for alleviation of adverse inlet spillage interactions with external stores (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Dan H. Neuhart, Matthew N. Rhode, and Langley Research Center (page images at HathiTrust)
• Aerodynamic performance of flared fan nozzles used as inlets (U.S. National Aeronautics and Space Administration ;, 1976), by Donald A. Dietrich, Gary G. Kelm, Theo G. Keith, and Lewis Research Center (page images at HathiTrust)
• Side forces on forebodies at high angles of attack and Mach numbers from 0.1 to 0.7 : two tangent ogives, paraboloid and cone (National Aeronautics and Space Administration ;, 1977), by Earl R. Keener and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine : II - effect of air ejection on turbine performance (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Jeffrey E. Haas, Milton G. Kofskey, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flow visualization studies of blowing from the tip of a swept wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Jeannette W. Smith, Dan H. Neuhart, Raymond E. Mineck, and Langley Research Center (page images at HathiTrust)
• Low-speed aerodynamic characteristics of a transport model having 42.33 ̊swept low wing with supercritical airfoil, double-slotted flaps, and T-tail or low tail (National Aeronautics and Space Administration ;, 1975), by Paul G. Fournier and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Clyde Hayes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Richard J. Re, Laurence D. Leavitt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Dynamic characteristics of a space-station solar wing array (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by John T. Dorsey, Harold G. Bush, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stability boundaries for systems with frequency-model feedback and complementary filter (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), by L. Keith Barker, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics (National Aeronautics and Space Administration ;, 1979), by David E. Reubush and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by David F. Fisher, David M. Richwine, John H. Del Frate, and Dryden Flight Research Facility (page images at HathiTrust)
• Inverse boundary-layer theory and comparsion with experiment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James E. Carter, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Experimental aerodynamic characteristics for slender bodies with thin wings at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 (National Aeronautics and Space Administration ;, 1976), by Leland H. Jorgensen, Michael H. Howell, and Ames Research Center (page images at HathiTrust)
• Experimental aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 (U.S. National Aeronautics and Space Administration ;, 1976), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
• Wind-tunnel investigation of an advanced general aviation canard configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Joseph R. Chambers, Thomas M. Moul, Long P. Yip, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Experimental evaluation of nacelle-airframe interference forces and pressures at Mach numbers of 0.9 to 1.4 (National Aeronautics and Space Administration ;, 1977), by Daniel P. Bencze, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic performance of 0.4066-scale model of JT8D refan stage (U.S. National Aeronautics and Space Administration ;, 1976), by Royce D. Moore, Edward R. Tysl, George Kovich, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Delma C. Freeman, Roger H. Fournier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• The aerodynamic performance of several flow control devices for internal flow systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by William T. Eckert, Kenneth W. Mort, Brian M. Wettlaufer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Approximation concepts for numerical airfoil optimization (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Garret N. Vanderplaats, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Ames Research Center (page images at HathiTrust)
• Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Richard J. Re, Bobby L. Berrier, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Leading-edge deflection optimization for a highly swept arrow-wing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Paul L. Coe, James W. Fenbert, Jarrett K. Huffman, Langely Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Use of constrained optimization in the conceptual design of a medium-range subsonic transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Steven M. Sliwa, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Structural Dynamics Division research and technology accomplishments for FY 1988 and plans for FY 1989. (Langley Research Center, 1989), by James E. Gardner, Langley Research Center. Structures and Dynamics Division, and Langley Research Center (page images at HathiTrust)
• Investigation of installation effects on single-engine convergent-divergent nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by James R. Burley, Bobby L. Berrier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged (U.S. National Aeronautics and Space Administration ;, 1976), by Jeffrey E. Haas, Milton G. Kofskey, United States National Aeronautics and Space Administration, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Effects of nacelle configuration/position on performance of subsonic transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by L. H. Bangert, D. K. Krivec, R. N. Segall, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lockheed-California Company (page images at HathiTrust)
• Subsonic sting interference on the aerodynamic characteristics of a family of slanted-base ogive-cylinders (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Colin P. Britcher, W. Allen Kilgore, Charles W. Alcorn, Langley Research Center, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (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)
• Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. Volume IV, Performance of jet-flapped blade (National Aeronautics and Space Administration ;, 1969), by James L. Bettner, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Performance comparisons of high mach number compressor rotor blading (National Aeronautics and Space Administration ;, 1968), by J. P. Gostelow, L. H. Smith, K. W. Krabacher, Lewis Research Center, General Electric Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flow and acoustic characteristics of subsonic and supersonic jets from convergent nozzle (National Aeronautics and Space Administration, 1970), by Henry T. Nagamatsu, M. S. Gill, R. E. Sheer, United States National Aeronautics and Space Administration, and General Electric Company. Research and Development Center (page images at HathiTrust; US access only)
• Operating capabilities of selected electric-arc reentry environment simulators. (National Aeronautics and Space Administration, 1964), by N. K. Hiester, Stanford Research Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Tests of a "D" vented thrust deflecting nozzle behind a simulated turbofan engine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by T. L. Watson, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment (National Aeronautics and Space Administration ;, 1971), by Paul M. Kenner, Ralph B. Holt, Frederic T. Churchill, United States National Aeronautics and Space Administration, Langley Research Center, and Vought Missiles and Space Division LTV Aerospace Corporation (page images at HathiTrust)
• Subjective reactions to sonic boom (National Aeronautics and Space Administration, 1965), by K. S. Pearsons, Karl D. Kryter, Beranek Bolt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A review of the planform effects on the low-speed aerodynamic characteristics of triangular and modified triangular wings (National Aeronautics and Space Administration, 1966), by Kenneth Razak and Melvin H. Snyder (page images at HathiTrust; US access only)
• Drag coefficients of microscopic spheres in free-molecule flow (National Aeronautics and Space Administration, 1967), by A. S. Hersh, J. C. Slattery, and J. F. Friichtenicht (page images at HathiTrust; US access only)
• Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method (National Aeronautics and Space Administration ;, 1975), by Larry Wayne Mohn, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• A theoretical method for the analysis and design of axisymmetric bodies (National Aeronautics and Space Administration ;, 1975), by T. D. Beatty, Langley Research Center, and McDonnell Douglas Corporation (page images at HathiTrust)
• Light aircraft lift, drag, and moment prediction : a review and analysis (National Aeronautics and Space Administration, 1975), by Frederick O. Smetana, Langley Research Center, and North Carolina State University (page images at HathiTrust)
• Vorticity interaction effects on blunt bodies (National Aeronautics and Space Administration ;, 1977), by E. Clay Anderson, David C. Wilcox, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The inviscid pressure field on the tip of a semi-infinite wing and its application to the formation of a tip vortex (National Aeronautics and Space Administration ;, 1976), by G. F. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Finite element analysis of low speed viscous and inviscid aerodynamic flows (National Aeronautics and Space Administration ;, 1977), by A. J. Baker and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattice method, L216 (DUBFLEX) (National Aeronautics and Space Administration ;, 1979), by M. Richard, B. A. Harrison, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• A computer program to generate equations of motion matrices, L217 (EOM). (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume II, Aerodynamics and aerodynamic loads (National Aeronautics and Space Administration ;, 1970), by James C. Williams, John N. Perkins, Delbert C. Summey, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Analysis of wing slipstream flow interaction (National Aeronautics and Space Administration, 1970), by Antony Jameson, United States National Aeronautics and Space Administration, Ames Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• NASA CR-1523 (National Aeronautics and Space Administration ;, 1970), by Richard F. Porter, Joe H. Brown, United States National Aeronautics and Space Administration, Ames Research Center, and Battelle Memorial Institute (page images at HathiTrust)
• An exploratory aerodynamic and structural investigation of all-flexible parawings (National Aeronautics and Space Administration, 1970), by J. N. Nielsen, United States National Aeronautics and Space Administration, and Nielsen Engineering & Research (page images at HathiTrust)
• A method of calculating wind tunnel interference factors for tunnels of arbitrary cross-section (National Aeronautics and Space Administration, 1967), by Robert G. Joppa (page images at HathiTrust; US access only)
• Wind tunnel interference factors for high-lift wings in closed wind tunnels (National Aeronautics and Space Administration, 1973), by Robert G. Joppa, Langley Research Center, and University of Washington (page images at HathiTrust)
• Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by John DeYoung, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Computation of three-dimensional nozzle-exhaust flow fields with the GIM code (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by L. W. Spradley, M. L. Pearson, P. G. Anderson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Application of the Bernoulli enthalpy concept to the study of vortex noise and jet impingment noise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by John E. Yates and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Analytical and experimental study of flow phenomena in noncavitating rocket pump inducers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by B. Lakshminarayana, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Investigations of simulated aircraft flight through thunderstorm outflows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Walter Frost and George C. Marshall Space Flight Center (page images at HathiTrust)
• Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience ; prepared for Langley Research Center under contract NAS1-15006. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by H. W. Mann, J. N. Ralston, C. W. Smith, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analytical study of a free-wing/free-trimmer concept (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Richard F. Porter, Battelle Memorial Institute. Columbus Laboratories, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Characteristics of dilute gas-solids suspensions in drag reducing flow (National Aeronautics and Space Administration, 1973), by Ronald Steven Kane (page images at HathiTrust; US access only)
• Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William G. Schweikhard, Yen-Sen Chen, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Subsonic panel method for designing wing surfaces from pressure distribution (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by D. R. Bristow, J. Dennis Hawk, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A geometry package for generation of input data for a three-dimensional potenial-flow program (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by N. Douglas Halsey, John L. Hess, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Homing performance comparison of selected airframe configurations using skid-to-turn and bank-to-turn steering policies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by R. T. Reichert, Johns Hopkins University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : User's manual (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Sedat Biringen, Oden J. McMillan, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Numerical analysis and FORTRAN program for the computation of the turbulent wakes of turbomachinery rotor blades, isolated airfoils and cascade of airfoils (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by C. Hah, B. Lakshminarayana, Pennsylvania State University. Dept. of Aerospace Engineering, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Stan J. Miley, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William Mulcay, Julio Chu, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Integrated application of active controls (IACC) technology to an advanced subsonic transport : project plan (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), by Boeing Commercial Airplane Company, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An analysis of the crossover between local and massive separation on airfoils (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by M. Burnett, J. E. Carter, and Langley Research Center (page images at HathiTrust)
• Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by William Bihrle, Robert Rose, William Mulcay, Randy S. Hultberg, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• General design method for three-dimensional potential flow fields (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by John D. Stanitz and Lewis Research Center (page images at HathiTrust)
• Aeroelastic addition to NASTRAN (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by William P. Rodden, E. Dean Bellinger, Robert L. Harder, and Langley Research Center (page images at HathiTrust)
• Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William Mulcay, Robert A. Rose, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Sedat Biringen, Oden J. McMillan, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Dual methods and approximation concepts in structural synthesis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Claude Fleury, Lucien André Schmit, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An exploratory investigation of the STOL landing maneuver (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Patrick H. Whyte, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An improved Woodward's panel method for calculating leading-edge and side-edge suction forces at subsonic and supersonic speed (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by C. Edward Lan, Sudhir C. Mehrotra, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Advanced missile technology : a review of technology improvement areas for cruise missiles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by L. L. Cronvich, H. P. Liepman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Characteristics of loaded fan rotor blade wakes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by B. Reynolds, B. Lakshminarayana, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A viscous flow analysis for the tip vortex generation process (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by S.J. Shamroth, W. R. Briley, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A comparison of the pitching and plunging response of an oscillating airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by F. O. Carta, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A three dimensional vortex wake model for missiles at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by J. Steven Sheffield, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Development of panel methods for subsonic analysis and design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by D. R. Bristow, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• The Influence of sweep on the aerodynamic loading of an oscillating NACA 0012 airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by A. O. St. Hilaire and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by John Kuhlmann, Michael J. Cerney, Paul Liaw, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Inverse design technique for cascades (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984), by Luca Zannetti, Maurizio Pandolfi, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Inc G.M.A.F. (page images at HathiTrust)
• Calculation of aerodynamic characteristics of airplane configurations at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Jing-Biau Tseng, C. Edward Lan, and Langley Research Center (page images at HathiTrust)
• Computer program to calculate three-dimensional boundary layer over wings with wall mass transfer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by J. D. McLean, J. L. Randall, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An approximate analytical method for studying entry into planetary atmospheres (U.S. G.P.O., 1959), by Dean R. Chapman, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Several methods for aerodynamic reduction of static-pressure sensing errors for aircraft at subsonic, near-sonic, and low supersonic speeds (U.S. G.P.O.], 1959), by Virgil S. Ritchie (page images at HathiTrust)
• Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data (U.S. G.P.O., 1962), by William R. Wells, William O. Armstrong, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Numerical results for the diffraction of a normal shock wave by a sphere and for the subsequent transient flow (National Aeronautics and Space Administration, 1967), by Richard W. Barnwell (page images at HathiTrust)
• Nearly circular transfer trajectories for descending satellites (U.S. G.P.O., 1959), by George M. Low, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Aerodynamic analysis of tektites and their parent bodies (National Aeronautics and Space Administration, 1962), by E. W. Adams and R. M. Huffaker (page images at HathiTrust)
• Experimental and theoretical studies of axisymmetric free jets (U.S. G.P.O., 1959), by Eugene S. Love, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A Theoretical study of stagnation-point ablation (U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Stagnation-point shielding by melting and vaporization (U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at Mach number from 1.57 to 2.86 (National Aeronautics and Space Administration :, 1963), by Dennis E. Fuller, Victor E. Langhans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Correlation of sonic-boom theory with wind-tunnel and flight measurements (National Aeronautics and Space Administration, 1964), by Harry W. Carlson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• NASA TR R-182 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), by Richard D. Wagner, Ralph Watson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TR R-183 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), by Robert J. Naumann, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed (National Aeronautics and Space Administration ;, 1963), by H. Jullian Allen, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Measured response to wind-induced dynamic loads of a full-scale scout vehicle mounted vertically on a launching tower (National Aeronautics and Space Administration :, 1961), by George W. Jones and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A three-dimensional trajectory simulation using six degrees of freedom with arbitrary wind,. (National Aeronautics and Space Administration :, 1961), by Robert L. Jr James and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TR R-101 (National Aeronautics and Space Administration :, 1961), by J. Richard Spahr and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-2380 (National Aeronautics and Space Administration :, 1964), by Raymond D. Vogler, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• NASA TN D-2340 (National Aeronautics and Space Administration :, 1964), by Earl A. Price, Robert L. Stallings, Paul W. Howard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-2483 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Lawrence W. Brown, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Lubricating oils for aviation gas turbines (National Aeronautics and Space Administration, 1960), by V. V. Panov, Yu. S. Sobolev, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3744 (National Aeronautics and Space Administration :, 1966), by Theodore A. Brabbs, Frank E. Belles, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamik; ein Gesamtwerk über das Fliegen (B.G. Teubner, 1909), by F. W. Lanchester, A. Runge, and Carl Runge (page images at HathiTrust; US access only)
• Survey of energy-absorption devices for soft landing of space vehicles (National Aeronautics and Space Administration :, 1962), by Jack B. Esgar and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5299 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Harold G. Gaidsick, Robert C. McCracken, William H. Dana, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 (National Aeronautics and Space Administration :, 1962), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4034 (National Aeronautics and Space Administration ;, 1967), by Lawrence E. Putnam, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5121 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by James C. Ellison, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flight investigation of V/STOL height-control requirements for hovering and low-speed flight under visual conditions (National Aeronautics and Space Administration, 1967), by James R. Kelly, Perry L. Deal, John F. Garren, and Langley Research Center (page images at HathiTrust)
• Analysis of melting boundary layers on decelerating bodies (National Aeronautics and Space Administration :, 1962), by Simon Ostrach, Jesse Hamman, Arthur W. Goldstein, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 (National Aeronautics and Space Administration :, 1960), by Harry L. Runyan, Nan H. Jones, and Langley Research Center (page images at HathiTrust)
• Fixed-base simulator study of the effect of time delays in visual cues on pilot tracking performance (National Aeronautics and Space Administration ;, 1975), by M. J. Queijo, Donald R. Riley, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6142 (National Aeronautics and Space Administration ;, 1971), by Richard J. Margason, John E. Lamar, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range (National Aeronautics and Space Administration ;, 1968), by Richard J. Margason, Garl L. Gentry, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Distribution of time-averaged pressure fluctuations along the boundary of a round subsonic jet (National Aeronautics and Space Administration :, 1960), by Walton L. Howes and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6003 (National Aeronautics and Space Administration :, 1970), by Moses G. Farmer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5951 (National Aeronautics and Space Administration :, 1970), by Joseph W. Cleary, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5921 (National Aeronautics and Space Administration :, 1970), by Joseph R. Chambers, James S. Bowman, Ernie L. Anglin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5885 (National Aeronautics and Space Administration :, 1970), by William J. Small, David E. Fetterman, Frank S. Kirkham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack (National Aeronautics and Space Administration ;, 1977), by James M. Luckring and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5434 (National Aeronautics and Space Administration ;, 1969), by L. Bernard Garrett, John N. Perkins, John T. Suttles, North Carolina State University, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft (National Aeronautics and Space Administration, 1970), by Kenneth W. Mort, Michael D. Falarski, U.S. Army Aeronautical Research Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical pressure distributions over arbitrarily shaped periodic waves in subsonic compressible flow, and comparison with experiment (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by K. R. Czarnecki and Mary W. Jackson (page images at HathiTrust; US access only)
• Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data (National Aeronautics and Space Administration ;, 1976), by Kenneth W. Iliff, Richard E. Maine, United States National Aeronautics and Space Administration, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• NASA TN D-4791 (National Aeronautics and Space Administration :, 1968), by Thomas E. Walton, Brian J. O'Hare, William G. Witte, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems (National Aeronautics and Space Administration ;, 1976), by Jules B. Dods, Earl C. Watson, Ames Research Center, and United States. National Aeronautics and Space Center (page images at HathiTrust)
• Effects of variable turbine area on subsonic cruise performance of turbojets designed for supersonic application (National Aeronautics and Space Administration :, 1970), by Arvid L. Keith, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5971 (National Aeronautics and Space Administration :, 1970), by Francis J. Capone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5940 (National Aeronautics and Space Administration :, 1970), by G. Kimball Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet (National Aeronautics and Space Administration ;, 1977), by Royce D. Moore, George W. Lewis, George Kovich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5900 (National Aeronautics and Space Administration :, 1970), by Blair B. Gloss, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles (National Aeronautics and Space Administration ;, 1974), by Vernard E. Lockwood, Aniello Matarazzo, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5901 (National Aeronautics and Space Administration :, 1970), by Charles G. Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5911 (National Aeronautics and Space Administration ;, 1970), by Harry L. Morgan, Charles F. Bradshaw, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 (National Aeronautics and Space Administration ;, 1968), by Odell A. Morris, Robert J. Mack, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5625 (National Aeronautics and Space Administration :, 1970), by Nestor Clough, Allen R. McMillan, Seymour Lieblein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5636 (National Aeronautics and Space Administration :, 1970), by James Wayne Sawyer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail (National Aeronautics and Space Administration, 1968), by Richard J. Margason, Garl L. Gentry, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical study of effects of severe turbulence on flight motions of a typical subsonic jet-transport airplane (National Aeronautics and Space Administration, 1969), by William D. Grantham, Mary S. Adams, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• 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)
• Effects of jet-exhaust location on the longitudinal aerodynamic characteristics of a jet V/STOL model (National Aeronautics and Space Administration ;, 1969), by Arthur W. Carter, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5714 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by George L. Von Pragenau, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4726 (National Aeronautics and Space Administration ;, 1968), by Delma C. Freeman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of V/STOL transport model with six wing-mounted lift fans (National Aeronautics and Space Administration, 1970), by William A. Newsom, Frederick L. Moore, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5344 (National Aeronautics and Space Administration ;, 1969), by John Zuk, Lawrence P. Ludwig, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effects of Reynolds number and body corner radius on aerodynamic characteristics of a space shuttle-type vehicle at subsonic Mach numbers (National Aeronautics and Space Administration, 1972), by Leland H. Jorgenson, Jack J. Brownson, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• NASA TN D-6636 (National Aeronautics and Space Administration :, 1972), by William A. Olsen, Robert G. Dorsch, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6643 (National Aeronautics and Space Administration :, 1972), by William T. Suit, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6655 (National Aeronautics and Space Administration :, 1972), by William H. Andrews, Richard R. Larson, Glenn H. Robinson, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions (National Aeronautics and Space Administration ;, 1972), by George C. Greene and Langley Research Center (page images at HathiTrust)
• Spherical balloon response to three-dimensional time-dependent flows (National Aeronautics and Space Administration ;, 1972), by George H. Fichtl and George C. Marshall Space Flight Center (page images at HathiTrust)
• Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10. (National Aeronautics and Space Administration :, 1970), by Robert I. Sammonds, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Review of propulsion-induced effects on aerodynamics of jet/stol aircraft (National Aeronautics and Space Administration :, 1970), by Richard J. Margason, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of Reynolds number on the lateral-stability derivatives at low speed of swept-back and delta-wing-fuselage combinations oscillating in yaw (National Aeronautics and Space Administration :, 1960), by Charles P. Llewellyn and Walter D. Wolhart (page images at HathiTrust)
• Investigation of aerodynamic effects of external combustion below flat-plate model in 10- by 10-foot wind tunnel at Mach 2.4 (National Aeronautics and Space Administration, 1960), by Robert G. Dorsch, Murray Dryer, Harrison Allen, and Lewis Research Center (page images at HathiTrust)
• Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing (National Aeronautics and Space Administration ;, 1969), by Marvin P. Fink, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Data from a static-thrust investigation of a large-scale general research vtol-stol model in ground effect (National Aeronautics and Space Administration :, 1960), by Robert J. Huston and Matthew M. Winston (page images at HathiTrust)
• Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing (National Aeronautics and Space Administration ;, 1973), by Bruce G. Powers, David A. Kier, and Flight Research Center (U.S.) (page images at HathiTrust)
• Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston. (National Aeronautics and Space Administration :, 1970), by Matthew M. Winston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Investigation of the flow over simple bodies at Mach numbers of the order of 20 (National Aeronautics and Space Administration :, 1960), by Arthur Henderson and Langley Research Center (page images at HathiTrust)
• Atomization, drop size, and penetration for cross-stream water injection at high-altitude reentry conditions with application to the RAM C-I and C-III flights (National Aeronautics and Space Administration ;, 1972), by Paul B. Gooderum, Dennis M. Bushnell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-1800 (National Aeronautics and Space Administration, 1963), by David J. Romeo, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4237 (National Aeronautics and Space Administration ;, 1967), by Kenneth W. Goodson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analysis of the limit-cycle and structural-resonance characteristics of the X-15 stability augmentation system (National Aeronautics and Space Administration, 1967), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Longitudinal aerodynamic characteristics in ground effect of a large-scale, V/STOL model with four tilting ducted fans arranged in a dual tandem configuration (National Aeronautics and Space Administration, 1967), by Demo J. Giullianetti, Ralph L. Maki, James C. Biggers, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 (National Aeronautics and Space Administration, 1960), by Victor L. Peterson, Loren G. Bright, and Ames Research Center (page images at HathiTrust)
• Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration (National Aeronautics and Space Administration, 1959), by William J. Alford, William P. Handerson, Arvo A. Luoma, and Langley Research Center (page images at HathiTrust)
• Systems identification using a modified Newton-Raphson method : A Fortran program (U.S. National Aeronautics and Space Administratration, 1972), by Lawrence W. Taylor and Kenneth W. Iliff (page images at HathiTrust)
• Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study (National Aeronautics and Space Administration ;, 1972), by Robert W. Rainey and Langley Research Center (page images at HathiTrust)
• Empirical three-sigma wind component profiles 45-degree missile flight azimuth Atlantic Missle Range PAtrick AFB (Cape Canaveral), Florida (National Aeronautics and Space Administration :, 1961), by William W. Vaughan (page images at HathiTrust)
• Automatic fixed camera orientation procedures (National Aeronautics and Space Administration :, 1961), by C. L. Bannister (page images at HathiTrust)
• Measurement of the maximum speed attained by the X-15 airplane powered with interim rocket engines (National Aeronautics and Space Administration :, 1960), by Wendell H. Stillwell and Terry J. Larson (page images at HathiTrust)
• NASA TN D-5468 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Kenneth W. Mort, Michael D. Falarski, Army Aeronautical Research Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5469 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John D. Warmbrod, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements (National Aeronautics and Space Administration, 1971), by W. Jefferson Stroud, Manuel Stein, Cornelia B. Dexter, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Full-scale wind-tunnel tests of a medium-weight utility helicopter at forward speeds (National Aeronautics and Space Administration :, 1963), by John L. McCloud, Ralph L. Maki, James C. Biggers, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6262 (National Aeronautics and Space Administration ;, 1971), by Kenneth K. Yoshikawa, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field (National Aeronautics and Space Administration ;, 1971), by E. B. Klunker, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Study of a guidance scheme using approximate solutions of trajectory equations to control the aerodynamic skip flight of a reentry vehicle (National Aeronautics and Space Administration :, 1963), by Robert S. Dunning and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Fortran program to calculate the flow field and performance of an axially symmetric deLaval nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1965), by D. Thompson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• External aerodynamics of the magnetosphere (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by John R. Spreiter, Audrey L. Summers, and Alberta Y. Alksne (page images at HathiTrust; US access only)
• Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 (National Aeronautics and Space Administration :, 1967), by James F. Campbell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3889 (National Aeronautics and Space Administration :, 1968), by Kenneth C. Weston, Manned Spacecraft Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Fatigue under random and programmed loads (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), by Eugene C. Naumann, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion (National Aeronautics and Space Administration :, 1960), by Thomas R. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3030 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), by Robert E. Reed, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1724 (National Aeronautics and Space Administration, 1963), by Terry J. Larson, Lannie D. Webb, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1629 (National Aeronautics and Space Administration, 1963), by Raymond D. Vogler, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel investigation of a deflected-slipstream cruise-fan V/STOL aircraft wing (National Aeronautics and Space Administration, 1967), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1624 (National Aeronautics and Space Administration, 1963), by Sandy M. Stubbs, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight (National Aeronautics and Space Administration, 1962), by Kenneth W. Goodson, Kalman J. Grunwald, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-1650 (National Aeronautics and Space Administration, 1963), by David H. Hickey, Leo P. Hall, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1628 (National Aeronautics and Space Administration, 1963), by P. Calvin Stainback, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Pressure distributions on 3 rigid wings simulating parawings with varied canopy curvature and leading-edge sweep at Mach numbers from 2.29 to 4.65 (National Aeronautics and Space Administration, 1963), by Paul G. Fournier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Large-scale wind-tunnel investigation of a model with an external jet-augmented flap (National Aeronautics and Space Administration, 1967), by Jerry V. Kirk, Kiyoshi Aoyagi, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1627 (National Aeronautics and Space Administration, 1963), by William Gracey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Empirical equation for turbulent forced-convection heat transfer for prandtl numbers from 0.001 to 1000 (National Aeronautics and Space Administration :, 1960), by Uwe H. VonGlahn and Lewis Research Center (page images at HathiTrust)
• Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model (National Aeronautics and Space Administration ;, 1969), by Matthew M. Winston, Robert J. Huston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of engine position and high-lift devices on aerodynamic characteristics of an external-flow jet-flap STOL model (National Aeronautics and Space Administration ;, 1971), by Charles C. Smith, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ (National Aeronautics and Space Administration :, 1963), by Charles D. Trescot, Cuyler W. Brooks, Lawrence E. Putman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ (National Aeronautics and Space Administration :, 1963), by Cuyler W. Brooks, Charles D. Trescot, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of the airflow over a cavity with antiresonance devices (National Aeronautics and Space Administration ;, 1971), by Donald A. Buell, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of peak deceleration on range sensitivity for a modulated-lift reentry at supercircular speeds (National Aeronautics and Space Administration :, 1963), by Charlie M. Jackson, Roy V. Harris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Trailblazer I reentry-body wind-tunnel tests at a Mach number of 6.7 with theoretical aerodynamics and a limited dynamic analysis (National Aeronautics and Space Administration :, 1963), by Herbert R. Schippell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed investigation of cable tension and aerodynamic characteristics of a parawing and spacecraft combination (National Aeronautics and Space Administration :, 1963), by William C. Sleeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6234 (National Aeronautics and Space Administration ;, 1971), by Stanley O. Dickinson, Brent K. Hodder, Leo P. Hall, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Full-scale wind-tunnel investigation on effects of slot spoilers on the aerodynamic characteristics of a light twin-engine airplane (National Aeronautics and Space Administration ;, 1973), by Harry A. Verstynen, Dominick Andrisani, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6687 (National Aeronautics and Space Administration :, 1972), by Edward L. Shriver, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0 degree to 90 degree (National Aeronautics and Space Administration, 1959), by Bernard Spencer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50 degree (National Aeronautics and Space Administration, 1960), by John B. McDevitt, John V. Rakich, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic (National Aeronautics and Space Administration ;, 1971), by Alan D. Levin, Ronald C. Smith, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration (National Aeronautics and Space Administration, 1960), by Gerald V. Foster, Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 (National Aeronautics and Space Administration, 1974), by Robert W. Kempel, John A. Manke, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of a coupled roll-spiral-mode, pilot-induced oscillation experienced with the M2-F2 lifting body (National Aeronautics and Space Administration, 1971), by Robert W. Kempel, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An exploratory investigation of the low-speed aerodynamic characteristics of variable-wing-sweep airplane configurations (National Aeronautics and Space Administration, 1959), by Williams J. Alford, William P. Handerson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : I. Subsonic (National Aeronautics and Space Administration ;, 1971), by Ronald C. Smith, Alan D. Levin, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : III. Supersonic (National Aeronautics and Space Administration ;, 1971), by Ronald C. Smith, Alan D. Levin, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model (National Aeronautics and Space Administration ;, 1973), by James L. Thomas, Delwin R. Croom, Danny R. Hoad, and Langley Research Center (page images at HathiTrust)
• A method for estimating static aerodynamic characteristics for slender bodies of circular and noncircular cross section alone and with lifting surfaces at angles of attack from 0 ̊to 90 ̊ (National Aeronautics and Space Administration ;, 1973), by Leland H. Jorgensen and Ames Research Center (page images at HathiTrust)
• NASA TN D-6321 (National Aeronautics and Space Administration ;, 1971), by William J. McCroskey, U.S. Army Air Mobility Research and Development Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations at Mach numbers from 1.60 to 2.86. (National Aeronautics and Space Administration :, 1971), by Samuel M. Dollyhigh, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a large-scale model a lift fan mounted in a 5-percent-thick triangular wing, including the effects of BLC on the lift-fan inlet (National Aeronautics and Space Administration, 1970), by Brent K. Hodder, Leo P. Hall, Jerry V. Kirk, United States National Aeronautics and Space Administration, U.S. Army Air Mobility Research and Development Laboratory, and Ames Research Center (page images at HathiTrust)
• De la locomotion mécanique dans l'air et dans l'eau (A. Bertrand, 1864), by Gustave Lambert (page images at HathiTrust)
• Solution du problème de la locomotion aérienne; aperçu général & sommaire, avec 21 figures à l'appui (Carilian-Gœury et V. Dalmont; [etc., etc.], 1853), by Michel Loup (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Carl Kaplan, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities (NACA, 1951), by L. G. Loĭt�si�anskiĭ and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Harry E. Murray, Clarence L. Gillis, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• The excitation of unstable perturbations (NACA, 1952), by J. Pretsch and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• General theory of conical flows and its application to supersonic aerodynamics (NACA, 1955), by Paul Germain and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transmission in the boundary layer (NACA, 1949), by L. E. |q Kalikhman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Development of a laminar boundary layer behind a suction point (NACA, 1952), by W. Wuest and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Concerning the flow about ring-shaped cowlings of finite thickness Part I (NACA, 1952), by Dietrich Küchemann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculation of the shape of a two-dimensional supersonic nozzle in closed form (NACA, 1953), by Dante Cunsolo and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Behavior of the laminar boundary layer for periodically oscillating pressure variation (NACA, 1949), by August Wilhelm Quick, K. Schröder, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On rotational conical flow (NACA, 1952), by Carlo Ferrari and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Concerning the flow about ring-shaped cowlings. Part VIII, further measurements on annular profiles (NACA, 1952), by Dietrich Küchemann, Johanna Weber, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Concerning the flow about ring-shaped cowlings. Part II, Annular bodies of infinite length with circulation for smooth entrance (NACA, 1951), by Dietrich Küchemann, Johanna Weber, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the turbulent friction layer for rising pressure (NACA, 1951), by K. Wieghardt, W. Tillmann, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Contributions to the theory of the spreading of a free jet issuing from a nozzle (NACA, 1951), by W. Szablewski and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theory of wing of circular plan form (NACA, 1953), by N. E. Kochin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Correction factors for wind tunnels of elliptic section with partly open and partly closed test section (NACA, 1951), by Friedrich Wilhelm Riegels and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The effect of high viscosity on the flow around a cylinder and around a sphere (NACA, 1952), by F. Homann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A simple numerical method for the calculation of the laminar boundary layer (National Advisory Committee for Aeronautics, 1952), by K. Schröder and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental determination of local and mean coefficients of heat transfer for turbulent flow in pipes (NACA, 1954), by I. T. Aladyev and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Spiral motions of viscous fluids (NACA, 1953), by Georg Hamel and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lift on a bent, flat plate (NACA, 1952), by F. Keune and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Air admixture to exhaust jets (NACA, 1953), by Eugen Sänger and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the design of airfoils in which the transition of the boundary layer is delayed (NACA, 1952), by Itiro Tani and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Concerning the flow about ring-shaped cowlings. Part XII, two new classes of circular cowls (NACA, 1953), by Dietrich Küchemann, Johanna Weber, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lame's wave functions of the ellipsoid of revolution (NACA, 1949), by J. Meixner and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On stability and turbulence of fluid flows (NACA, 1951), by Werner Heisenberg and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some experiences regarding the nonlinearity of hot wires (NACA, 1952), by Robert Betchov, W. Welling, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On a class of exact solutions of the equations of motion of a viscous fluid (NACA, 1953), by V. I. Yatseyev and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Concerning the flow about ring-shaped cowlings. Part XIII, the influence of a projecting hub (NACA, 1953), by Dietrich Küchemann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Determination of the stress concentration factor of a stepped shaft stressed in torsion by means of precision strain gages (NACA, 1947), by A. Weigand and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Resistance of cascade of airfoils in gas stream at subsonic velocity (NACA, 1951), by L. G. Loĭt�si�anskiĭ and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On motion of fluid in boundary layer near line of intersection of two planes (NACA, 1951), by L. G. Loĭt�si�anskiĭ, V. P. Bolshakov, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On combustion in a turbulent flow (NACA, 1947), by K. I. Shelkin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Infinitesimal conical supersonic flow (NACA, 1947), by Adolf Busemann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculation of turbulent expansion processes (NACA, 1945), by Walter Tollmien and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lecture series "boundary layer theory." Part II, turbulent flows (NACA, 1949), by H. Schlichting and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The plane problem of the flapping wing (NACA, 1954), by Walter Birnbaum and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A new simple interferometer for obtaining quantitatively evaluable flow patterns (NACA, 1953), by S. F. Erdmann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• General characteristics of the flow through nozzles at near critical speeds (NACA, 1947), by R. Sauer and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the application of the energy method to stability problems (NACA, 1947), by K. Marguerre and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The elliptic wing based on the potential theory (NACA, 1941), by Klaus Krienes and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• An approximate method for calculation of the laminar boundary layer with suction for bodies of arbitrary shape (NACA, 1949), by H. Schlichting and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The flow of gases in narrow channels (NACA, 1951), by R. E. H. Rasmussen and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Jet diffusion in proximity of a wall (NACA, 1949), by D. Küchemann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the theory of the Laval nozzle (NACA, 1949), by S. V. Falkovich and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Compression shocks in two-dimensional gas flows (NACA, 1949), by Adolf Busemann, J. Vanier, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Nonstationary gas flow in thin pipes of variable cross section (NACA, 1948), by G. Guderley, Dave Feingold, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Jerry Goodman, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Experimental study of flow past turbine blades (NACA, 1949), by E. Eckert, K. von Vietinghoff-Scheel, J. Vanier, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gas motion in a local supersonic region and conditions of potential-flow breakdown (NACA, 1949), by A. A. Nikol§skiĭ, G. I. Taganov, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Problem of slip flow in aerodynamics (National Advisory Committee for Aeronautics, 1957), by Robert E. Street and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Preliminary report on a study of separated flows in supersonic and subsonic streams (National Advisory Committee for Aeronautics, 1956), by Dean R. Chapman, Howard K. Larson, Donald M. Kuehn, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Formation of a vortex at the edge of a plate (NACA, 1956), by Leo Anton and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Laminar flow about a rotating body of revolution in an axial airstream (NACA, 1956), by H. Schlichting and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the problem of gas flow over an infinite cascade using Chaplygin's approximation (NACA, 1951), by G. A. Bugaenko and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the contribution of turbulent boundary layers to the noise inside a fuselage (NACA, 1956), by G. M. Corcos, H. W. Liepmann, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Approximate method of integration of laminar boundary layer in incompressible fluid (NACA, 1951), by L. G. Loĭt�si�anskiĭ and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the spectrum of natural oscillations of two-dimensional laminar flows (NACA, 1957), by D. Grohne and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Concerning the flow about ring-shaped cowlings. Part IX, The influence of oblique oncoming flow on the incremental velocities and air forces at the front part of circular cowls (National Advisory Committee for Aeronautics, 1952), by Dietrich Küchemann, Johanna Weber, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The problem of torsion in prismatic members of circular segmental cross section (NACA, 1948), by A. Weigand and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the statistical theory of turbulence (National Advisory Committee for Aeronautics, 1958), by Werner Heisenberg and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel corrections at high subsonic speeds particularly for an enclosed circular tunnel (NACA, 1952), by B. Göthert and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Boundary layer (National Advisory Committee for Aeronautics, 1956), by L. G. Loĭt�si�anskiĭ and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Extension to the cases of two dimensional and spherically symmetric flows of two particular solutions to the equations of motion governing unsteady flow in a gas (NACA, 1952), by Lorenzo Poggi and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The elasto-plastic stability of plates (NACA, 1947), by A. A. Il§i�ushin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Systematic investigations of the influence of the shape of the profile upon the position of the transition point (NACA, 1947), by K. Bussmann, A. Ulrich, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigations of the boundary-layer control on a full scale swept wing with air bled off from the turbojet (NACA, 1952), by Pierre Rebuffet, Ph. Poisson-Quinton, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A flat wing with sharp edges in a supersonic stream (NACA, 1956), by A. E. Donov and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Autogenous welding in airplane construction (NACA, 1929), by Ludwig Kuchel and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gas flow with straight transition line (NACA, 1951), by L. V. Ovsi�annikov and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the representation of the stability region in oscillation problems with the aid of the Hurwitz determinants (NACA, 1952), by E. Sponder and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight-velocity (Boysen & Maasch;, 1906), by Arnold Samuelson (page images at HathiTrust; US access only)
• Die Gesetze des Gleichgewichts und der Bewegung flüssiger Körper (Bey Siegfried Lebrecht Crusius, 1806), by Leonhard Euler and H. W. Brandes (page images at HathiTrust)
• Die Luft in Lichte der Lüftungstechnik. (C. Marhold, 1913), by Johannes Kelling (page images at HathiTrust; US access only)
• The aerodynamic analysis of single and multiple vehicles [entering and traveling in open tunnels] (Dept. of Transportation, Federal Railroad Administration, Office of Research, Development, and Demonstration ;, 1976), by Charles R. Strom, Development and Demonstration United States. Federal Railroad Administration. Office of Research, and Mitre Corporation (page images at HathiTrust)
• Aircraft vortex wake decay near the ground (U.S. Department of Transportation, Federal Aviation Administration, Systems Research and Development Service ;, 1977), by S. J. Barker, J. B. Mullen, P. B. S. Lissaman, I. Tombach, United States. Federal Aviation Administration. Systems Research and Development Service, Poseidon Research, and AeroVironment Inc (page images at HathiTrust)
• Aerodynamics; constituting the first volume of a complete work on aerial flight. (Constable, 1911), by F. W. Lanchester (page images at HathiTrust)
• Applied aerodynamics (New York, 1919), by G. P. Thomson (page images at HathiTrust; US access only)
• Essais d'aérodynamique. ([s.n.], 1911), by Armand Antoine Agénor de Gramont (page images at HathiTrust; US access only)
• An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect (National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ;, 1982), by John W. Paulson, Scott O. Kjelgaard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location (National Aeronautics and Space Administration, 1960), by Ralph P. Bielat, P. Kenneth Pierpont, and Langley Research Center (page images at HathiTrust)
• Effect of nozzle inlet geometry on performance of a swiveled convergent-divergent nozzle (National Aeronautics and Space Administration, 1959), by Albert J. Pavli and Lewis Research Center (page images at HathiTrust)
• Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor (National Aeronautics and Space Administration, 1959), by Ralph L. Schacht, Arthur W. Goldstein, Richard R. Cullom, and Lewis Research Center (page images at HathiTrust)
• Force, moment, and flow-field characteristics of two wing-body-nacelle combinations at Mach numbers 2 and 3 (National Aeronautics and Space Administration, 1960), by Jr. Hill and Ames Research Center (page images at HathiTrust)
• Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 (National Aeronautics and Space Administration, 1959), by Cornelius Driver and Langley Research Center (page images at HathiTrust)
• Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage (National Aeronautics and Space Administration, 1961), by Thomas G. Gainer and Langley Research Center (page images at HathiTrust)
• Transonic flutter investigation of models of the X-15 airplane horizontal tail (National Aeronautics and Space Administration, 1961), by Lou S. Young, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90 degrees (National Aeronautics and Space Administration, 1961), by John E. Grimaud and Langley Research Center (page images at HathiTrust)
• Full-scale wind-tunnel investigation of the low-speed static aerodynamic characteristics of a model of a reentry capsule (National Aeronautics and Space Administration, 1959), by William I. Scallion and Langley Research Center (page images at HathiTrust)
• Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 (National Aeronautics and Space Administration, 1959), by Jr. Stallings, Paige B. Burbank, and Langley Research Center (page images at HathiTrust)
• Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane (National Aeronautics and Space Administration, 1960), by Jim A. Penland, Jr. Fetterman, and Langley Research Center (page images at HathiTrust)
• Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle (National Aeronautics and Space Administration, 1960), by John P. Mugler, Walter B. Olstad, and United States National Aeronautics and Space Administration (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)
• 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)
• 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)
• Low-speed characteristics in pitch of a 34⁰ sweptforward wing with circular-arc airfoil sections (National Advisory Committee for Aeronautics, 1947), by D. William Conner, Patrick A. Cancro, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Sound measurements for five shrouded propellers at static conditions (National Advisory Committee for Aeronautics, 1949), by Harvey H. Hubbard, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 (National Advisory Committee for Aeronautics, 1952), by Bernard N. Daley, Richard S. Dick, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• 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), by Melvin M. Carmel, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• 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), by Edward Widmayer, Sumner A. Leadbetter, Sherman A. Clevenson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), by Edward C. Polhamus, William C. Sleeman, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• 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), by Douglas R. Lord, Robert Moring, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• 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), by Richard E. Kuhn, Andrew L. Byrnes, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• 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), by James W. Wiggins, Richard E. Kuhn, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Appraisal of method of flutter analysis based on chosen modes by comparison with experiment for cases of large mass coupling (National Advisory Committee for Aeronautics, 1949), by Donald S. Woolston, Harry L. Runyan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results (National Advisory Committee for Aeronautics, 1950), by John D. Bird, Byron M. Jaquet, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds (National Advisory Committee for Aeronautics, 1951), by John DeYoung and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Reciprocity relations in aerodynamics (National Advisory Committee for Aeronautics, 1952), by Max A. Heaslet, John R. Spreiter, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip (National Advisory Committee for Aeronautics, 1953), by Donald R. Riley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds (National Advisory Committee for Aeronautics, 1953), by Harvard Lomax 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)
• Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90©� (National Advisory Committee for Aeronautics, 1954), by John W. Draper, Richard E. Kuhn, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades (National Advisory Committee for Aeronautics, 1951), by William R. Slivka, David H. Silvern, Lewis Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Report on the theory of a stream line past a plane barrier : and of the discontinuity arising at the edge, with an application of the theory to an aeroplane (H.M.S.O., 1910), by G. Greenhill (page images at HathiTrust)
• Theory of a stream line past a curved wings (H. M. Stationery off., Sir J. Causton and sons, limited [printers], 1916), by G. Greenhill (page images at HathiTrust)
• The subsonic aerodynamic characteristics of some blunt delta configurations with 75° sweepback (National Aeronautics and Space Administration, 1961), by George G. Edwards, Howard F. Savage, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds (National Aeronautics and Space Administration, 1962), by Frank A. Lazzeroni and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle (National Aeronautics and Space Administration, 1962), by James L. Hassell, George M. Ware, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of wing-crank, leading-edge chord extensions and horizontal-tail height on the longitudinal stability of swept-wing models at mach numbers from 0.6 to 1.4 (National Aeronautics and Space Administration, 1959), by Roy M. Wakefield and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An investigation at subsonic speeds of the longitudinal aerodynamic characteristics at angles of attach from -4° to 100° of delta-wing reentry configurations having vertically displaced and cambered wing-tip panels (National Aeronautics and Space Administration, 1961), by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 (National Aeronautics and Space Administration, 1961), by Fred A. Demele, Jack J. Brownson, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation at Mach numbers of 0.20 to 3.50 of blended wing-body combinations of sonic design with diamond, delta and arrow plan forms (National Aeronautics and Space Administration, 1960), by George H. Holdaway, Jack A. Mellenthin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of blended wing-body combinations with curved plan forms at Mach numbers up to 3.50 (National Aeronautics and Space Administration, 1960), by George H. Holdaway, Jack A. Mellenthin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerial flight. (Van Nostrand, 1909), by F. W. Lanchester (page images at HathiTrust)
• Oberflachenrauhigkeiten auf Tragflugeln. (National Advisory Committee for Aeronautics ;, 1926), by O. Schrenk and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analysis of vane-type air motors (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1957), by B. Kaplan and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
• Die Flugmaschine : des dynamischen Flugprincipes in ihrer Ausfuhrung und Verwendung (W. Braumüller, 1898), by Eduard Mánfai (page images at HathiTrust)
• Aerodonetics : constituting the second volume of a complete work on aerial fight (Constable, 1917), by F. W. Lanchester (page images at HathiTrust; US access only)
• The mechanical principles of the aeroplane (Macmillan, 1921), by Selig Brodetsky (page images at HathiTrust)
• A slide rule type of device to measure logarithmic decay times as presented by oscillograph records (Sandia Corporation ;, 1960), by Rodman Leach, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
• Viscous flow past a rotating translating blade with arbitrary velocity suction and slip (U) (Sandia Corporation, 1963), by K. J. Touryan, Sandia Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust; US access only)
• Analytical determination of flight characteristics of aircraft (Sandia Corporation ;, 1959), by Alphonse Iacoletti and Sandia Corporation (page images at HathiTrust; US access only)
• The mechanics of the aeroplane : a study of the principles of flight. (Longmans, Green and co., 1917), by Emile Duchêne, T. O'B. Hubbard, and J. H. Ledeboer (page images at HathiTrust; US access only)
• Meteorology and aeronautics. (Govt. Printing Office., 1917), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Survey of methods for the determination of the subsonic flow characteristics of heated gases (Livermore Research Laboratory, 1952), by James Earle Mahlmeister, M. F. Katzer, Lawrence Livermore Laboratory, California Research and Development Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A compilation of longitudinal aerodynamic characteristics including pressure information for sharp-and blunt-nose cones having flat and modified bases (Sandia Corporation, 1965), by A. D. Foster, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• The Effect of simulated icing on propeller performance (National Advisory Committee for Aeronautics ;, 1946), by Blake W. Corson, Julian D. Maynard, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight measurements of the flying qualities of five light airplanes (National Advisory Committee for Aeronautics, 1948), by Paul A. Hunter and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• An introduction to aerodynamic stability (Sandia Corporation ;, 1957), by Paul W. Rowe and Sandia Corporation (page images at HathiTrust)
• Theoretical investigation at subsonic speeds of the flow ahead of a slender inclinded parabolic-arc body of revolution and correlation with experimental data obtained at low speeds (National Advisory Committee for Aeronautics, 1954), by William Letko, Edward C. B. Danforth, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The determination of aerodynamic stability coefficients from rocket flight test data (Sandia Corporation ;, 1961), by A. C. Bustamante and Sandia Corporation (page images at HathiTrust)
• Chord-wise air load distribution : War Dept., Army Air Forces : Navy Dept., Bureau of Aeronautics : Dept. of Commerce, Civil Aeronautics ... ([U.S. Govt. Print. Off.?], 1942), by United States. Army-Navy-Civil Committee on Aircraft Design Criteria (page images at HathiTrust)
• Aero-forces acting on a blunt body with separated flow (1962), by Yun-Sing Yuen (page images at HathiTrust; US access only)
• Aerodynamic forces on freight trains (Dept. of Transportation, Federal Railroad Administration, Office of Freight Systems ;, 1978), by Prakash B. Joshi and United States. Federal Railroad Administration. Office of Freight Systems (page images at HathiTrust)
• Unsteady aerodynamic forces on subsonic aircraft exposed to blast gusts of arbitrary orientation (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1958), by Robert F. Smiley and Eugene L. Krasnoff (page images at HathiTrust)
• A mathematical investigation of water droplet trajectories (Army Air Forces Headquarters, Air Technical Service Command ;, 1946), by Irving Langmuir, Katherine Blodgett, and United States. Army Air Forces (page images at HathiTrust)
• U.S.A. wing and propeller sections and biplane wing combinations. (Dayton, Ohio : Airplane Engineering Department, 1918., 1918), by United States. Bureau of Aircraft Production (page images at HathiTrust)
• Lautaret engine tests. (Dayton, Ohio : Airplane Engineering Department, 1918., 1918), by United States. Bureau of Aircraft Production (page images at HathiTrust)
• Section technique aeronautique radiator tests (Dayton, Ohio : Airplane Engineering Department, 1918., 1918), by United States. Bureau of Aircraft Production (page images at HathiTrust)
• Scientific fairing of veneer fuselages. (Dayton, Ohio : Airplane Engineering Division, Experimental Department, 1918., 1918), by United States. Bureau of Aircraft Production (page images at HathiTrust)
• Applied aeronautics (The Joseph G. Branch Pub. Co., 1943), by Joseph G. Branch (page images at HathiTrust; US access only)
• Aerodynamics for naval aviators (Office of the Chief of Naval Operations, Aviation Training Division, 1965), by Hugh H. Hurt and United States Office of the Chief of Naval Operations (page images at HathiTrust)
• Aerodynamic derivatives for both steady and non-steady motion of slender bodies (Aberdeen, Maryland : Aberdeen Proving Ground, 1955., 1955), by R. M. Wood, C. H. Murphy, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A study of artillery shell drift at high angle of fire using solar aspect sensors (Aberdeen, Maryland : Aberdeen Proving Ground, 1972., 1972), by W. Z. Collings, R. F. Lieske, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flow of heated gases (Los Angeles, California : North American Aviation, Inc., 1947., 1947), by A. S. Thompson, North American Aviation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flow of gases in constant-area passages with friction and arbitrary heat addition (Downey, California : Atomic Energy Research Department, North American Aviation, Inc., 1952., 1952), by M. P. Heisler, E. Martin, H. Sletten, U.S. Atomic Energy Commission, and North American Aviation (page images at HathiTrust)
• Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination (Washington, D.C. : National Advisory Committee for Aeronautics, [1955], 1955), by William J. Alford, Thomas J. King, H. Norman Silvers, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Notes on a series of lectures in theoretical aerodynamics ([Langley Field, VA, 1950), by Gilford Norman Ward and Morton Cooper (page images at HathiTrust; US access only)
• Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows (Department of Aeronautical Engineering, Massachusetts Institute of Technology, 1954), by Herbert M. Voss, Garabed Zartarian, Pao Tan Hsu, and Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust; US access only)
• Oscillatory aerodynamic loads on low-aspect-ratio wings in subsonic flow. (s. n.], 1955), by Massachusetts Institute of Technology. Aerolastic and Structures Research (page images at HathiTrust; US access only)
• An introduction to the aerodynamics of the airplane (part 2) (Rose Company, 1949), by H. Serbin (page images at HathiTrust; US access only)
• A detailed development of the tricyclic theory (Sandia Laboratories], 1968), by Harold R. Vaughn and Sandia Corporation (page images at HathiTrust; US access only)
• A laminar theory of the flow through a turbo-machine. (Rensellaer Polytechnic Institute, 1950), by Fausto G. Gravalos (page images at HathiTrust; US access only)
• Airfoil section data obtained in the N. A. C. A. variable-density tunnel as affected by support interference and other corrections (U. S. Govt. print. off.], 1939), by Eastman Nixon Jacobs and Ira Herbert Abbot (page images at HathiTrust; US access only)
• Théorie générale des régimes de l'aéroplane. (Paris, 1913), by Georges de Bothezat (page images at HathiTrust; US access only)
• Dynamical mechanisms producing large-scale transport of atmospheric trace substances (Naval Postgraduate School, 1970), by J. D. Mahlman and Naval Postgraduate School (U.S.) (page images at HathiTrust)
• Theory of flight (GPO, 1941), by United States War Department (page images at HathiTrust)
• Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration : report to the Committee on Science and Technology, House of Representatives (U.S. General Accounting Office, 1976), by United States General Accounting Office and United States. Congress. Senate. Committee on Science and Technology (page images at HathiTrust)
• Aerodynamics of the model airplane (Redstone Arsenal, Ala. : Translation Branch, Redstone Scientific Information Center, Research and Development Directorate, U.S. Army Missile Command, 1967-, 1967), by Franz Wilhelm Schmitz (page images at HathiTrust; US access only)
• Propagation of density disturbances in air-water flow (Evanston, Ill., 1965), by George Peter Nassos (page images at HathiTrust)
• The Coanda effect (U.S. Atomic Energy Commission, Technical Information Service, 1959), by U.S. Atomic Energy Commission, Albert Metral, and Friedrich Zerner (page images at HathiTrust)
• Reduction of incremental load factor acceleration data to gust statistics (FAA Technical Center ;, 1994), by J. B. de Jonge, Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), Federal Aviation Administration Technical Center (U.S.), and Netherlands. Rijksluchtvaartdienst (page images at HathiTrust)
• A computer program to obtain time-correlated gust loads for nonlinear aircraft using the matched-filter-based method (Federal Aviation Administration Technical Center ;, 1994), by Robert C. Scott, Boyd Perry, Anthony S. Pototzky, Langley Research Center. Aeroelasticity Branch, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Reanalysis of European flight loads data (FAA Technical Center ;, 1994), by J. B. de Jonge, P. A. van Gelder, P. A. Hol, Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Variation in load factor factor experience of Fokker F27 and F28 operational acceleration exceedance data (Federal Aviation Administration, Office of Aviation Research ;, 1996), by J. B. de Jonge, P. A. Hol, Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), and United States. Office of Aviation Research (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)
• Structural weight analysis; general method: wing structures. (Rand Corp., 1949), by F. R. Shanley and Rand Corporation (page images at HathiTrust; US access only)
• Aerodynamics of the oscillating air-foil in compressible flow ... (U.S. Headquarters air materiel command, 1947), by Samuel Noah Karp, Herschel Weil, and Shien Siu Shu (page images at HathiTrust; US access only)
• Perforated transonic wind tunnel walls (Providence, 1954), by P. F. Maeder (page images at HathiTrust; US access only)
• Les coefficients caractéristiques des turbo-machines et des machines volantes. (Paris, 1928), by Wladimir Margoulis (page images at HathiTrust; US access only)
• Mass unbalance in a simplified autospin system (Dept. of Theoretical and Applied Mechanics, University of Illinois, 1962), by John M. Doyle, Redstone Arsenal, and University of Illinois (Urbana-Champaign campus). Dept. of Theoretical and Applied Mechanics (page images at HathiTrust; US access only)
• Technische berichte ([London?], 1925), by Aerodynamische Versuchsanstalt Göttingen and Great Britain. Air Ministry (page images at HathiTrust; US access only)
• Handbook of inviscid sphere-cone flow fields and pressure distributions (White Oak, Silver Spring, Marlyand : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by A. M. Morrison, Naval Surface Weapons Center. White Oak Laboratory, R. E. Ferguson, M. Ciment, and J. M. Solomon (page images at HathiTrust)
• Handbook of blunt-body aerodynamics: volume 1 - static stability. (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1973., 1973), by John A. Darling and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Interacting supersonic turbulent boundary layers over a two-dimensional protuberance. (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1974., 1974), by Arnold Polak and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Two-component force balance for measuring skin friction and side force (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by Eugene V. Horanoff, Richard T. Driftmyer, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Passive aerodynamic attitude stabilization of near earth satellites (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1961., 1961), by United States. Air Force. Air Force Systems Command. Aeronautical Systems Division, O. C. Juelich, Paul H. Davidson, D. M. Schrello, and Wright Air Development Division (page images at HathiTrust)
• Final report on extraction of aircraft stability coefficients from flight test data and theoretical and experimental studies on selected problems of high speed aerodynamics and dynamic stability (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by Lloyd E. Wilkie, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Performance of trailing aerodynamic decelerators at high dynamic pressures : Phases V and VI (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1962., 1962), by B. A. Engstrom, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Solution of the potential equation for the unsteady flow about a triangular wing with subsonic leading edges in a supersonic main stream (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1957., 1957), by Yudell L. Luke, Frank Wagner, Geraldine V. Coombs, United States. Air Force. Air Research and Development Command, Midwest Research Institute, and Wright Air Development Center (page images at HathiTrust)
• Drag due to lift of a not-so-slender configuration (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1957., 1957), by Hsien K. Cheng, United States. Air Force. Air Research and Development Command, Inc Cornell Aeronautical Laboratory, and Wright Air Development Center (page images at HathiTrust)
• L'aviation; ses debuts--son développement (Berger-Levrault & cie, 1908), by Ferdinand Ferber (page images at HathiTrust; US access only)
• The theory of analysis and prediction of trajectories : final report (Texas A & M University, Dept. of Oceanography, 1958), by Texas A & M University System. Dept. of Oceanography, Guy A. Franceschini, and Texas A. and M. Research Foundation (page images at HathiTrust; US access only)
• Wing roll control devices for transonic high lift conditions. Part I, Fixed wing configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by Jack D. McAllister, Perry D. Whitten, David B. Benepe, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Mach 0.6 to 3.0 flows over rectangular cavities (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Louis G. Kaufman, Rodney L. Clark, Algirdas Maciulaitis, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aerospace Corporation. Research and Development Center (page images at HathiTrust)
• Low speed aerodynamics for ultra-quiet flight (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by R. A. Kroeger, T. C. Helvey, H.D. Gruschka, Air Force Flight Dynamics Laboratory (U.S.), and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Hybrid aerodynamic methods (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by Frank A. Dvorak, Donald W. Roberts, Gerald C. Paynter, T. S. Vaidyanathan, James K. Nathman, Brian Maskew, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), Boeing Military Airplane Company, and Inc Analytical Methods (page images at HathiTrust)
• Determining air reactions on moving vehicles (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957-., 1957), by Zbigniew Krzywoblocki, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and University of Chicago. Institute for System Research (page images at HathiTrust)
• Wing roll control devices for transonic high lift conditions. Part II, Variable sweep configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by Jack D. McAllister, Perry D. Whitten, David B. Benepe, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Thermal effects on static aeroelastic stability and control : description and results of tests conducted to determine the thermally affected deflectional behavior of corrugated multiweb wing structures (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Aeromechanics Branch, Air Research and Development Command, United States Air Force, 1959., 1959), by James F. Quinn, Richard H. Gallagher, Donald Turrentine, Bell Aircraft Corporation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• The effects of time-varying aerodynamic coefficients on aeroelastic response (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Richard H. MacNeal, Bernard Mazelsky, Jack H. Hill, Aerospace Medical Laboratory, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Development of an empirically based computer program to predict the aerodynamic characteristics of aircraft. Volume I, Basic Theoretical methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by M. L. Goldhammer, C. C. Shen, M. L. Lopez, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• Evaluations of methods to predict flutter of wings with external stores (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by Sidney Siegel, Lowell V. Andrew, Air Force Flight Dynamics Laboratory (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Exact vorticity solutions of the incompressible Navier-Stokes equations (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Aerodynamic analysis of a fighter aircraft with a higher order paneling method (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by A. R. Dusto, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Boeing Military Airplane Company (page images at HathiTrust)
• The drag of cones, plates, and hemispheres in the wake of a forebody in subsonic flow (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Helmut G. Heinrich, Eugene L. Haak, University of Minnesota. Department of Aerospace Engineering and Mechanics, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Two-dimensional supersonic nonadiabatic flow and axisymmetric supersonic adiabatic and nonadiabatic flows (Wright-Patterson Air Force Base, Ohio : b Air Force Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1966., 1966), by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, Wright-Patterson Air Force Base (Ohio), Itek Corporation, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Correlation of aerodynamic stability and control derivatives obtained from flight tests and wind tunnel tests on the XC-142A airplane (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Ernest L. Black, George C. Booth, Air Force Flight Dynamics Laboratory (U.S.), and LTV Aerospace Corporation (page images at HathiTrust)
• Tests to determine subsonic aerodynamic characteristics of hypersonic re-entry configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by K. Mantz, R. Ross, D. B. Seager, Aeronautical Systems Center (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Lockheed-California Company (page images at HathiTrust)
• A Source-Doublet approach to modeling triple ejector rack store configurations and force calculations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by Calvin L. Dyer, Charles B. Heath, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• A measurement of the static aeroelastic deformation and loading of a wing in supersonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Frank H. Durgin, C. J. Bartlett, United States. Air Force. Systems Command. Research and Technology Division, United States. Air Force. Systems Command. Aeronautical Systems Division, Massachusetts Institute of Technology, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Operating points, particle dynamics, and coordinate systems for aerospace vehicle stability and control (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Duane T. McRuer, Irving Ashkenas, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Subsonic flutter characteristics of a variable sweep wing and horizontal tail combination (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by Walter J. Mykytow, Michael H. Shirk, Lawrence J. Huttsell, Thomas E. Noll, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Response of aircraft encountering aircraft wake turbulence (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Robert C. Nelson and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Flow of a gas in a local supersonic zone and some conditions for the breakdown of potential flow (Graduate Division of Applied Mathematics, Brown University, 1948), by Alexander A. Nikolsky and G. I. Taganoff (page images at HathiTrust)
• Aerodynamic interference of wing-pylon-body combinations at low subsonic speeds (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Kenneth Boland Walkley, Fred W. Martin, United States. Air Force. Systems Command, Air Force Armament Laboratory, and Auburn University. Department of Aerospace Engineering (page images at HathiTrust)
• Numerical analysis of turbulent separated subsonic diffuser flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by J. C. Chien, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• Fluidic virtual aerosurfaces for flow control applications (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2004., 2004), by Ari Glezer, George W. Woodruff School of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• The compressible viscous layer in rarefied hypersonic flow (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Hung-Ta Ho, Ronald F. Probstein, United States. Air Force. Aeronautical Research Laboratories, and Brown University. Division of Engineering (page images at HathiTrust)
• Considerations on the structure of mixed subsonic-supersonic flow patterns (Wright Field, Dayton, Ohio : Headquarters Air Materiel Command, 1947., 1947), by Karl Gottfried Guderley and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Summary of instrumentation development and aerodynamic research in a hypersonic shock tunnel. Part II, Nozzle flow study and flow angularity measurements (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Charles E. Wittliff, Merle R. Wilson, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Parallel simulation of moving boundary flow using overset adaptive cartesian/prism grids and DES (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2004., 2004), by Z. J. Wang, Michigan State University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Aerodynamic/dynamic interaction (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1990., 1990), by Dean T. Mook, Ali Hasan Nayfeh, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Department, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Prediction of forces and moments on finned missiles at high angle of attack in transonic flow (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Division, Air Force Systems Command, United States Air Force, 1980., 1980), by William L. Oberkampf, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)
• AEDC high alpha aerodynamics. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), by Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• An experimental study of boattail pressures at high subsonic Mach numbers and high Reynolds numbers (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Systems Command, 1975., 1975), by John D. Lee, Aerospace Research Laboratories (U.S.), and Ohio State University. Research Foundation (page images at HathiTrust)
• Post stall maneuvers and thrust vectoring performance analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by L. Earl Miller, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Interactive plotting of NASTRAN aerodynamic models using NPLOT and DISSPLA (Kirtland Air Force Base, New Mexico : Air Force Weapons Laboratory, Air Force Systems Command, United States Air Force, 1988., 1988), by Steven G. Harris and United States. Air Force. Air Force Weapons Laboratory (page images at HathiTrust)
• Asymptotic far field conditions for unsteady subsonic and transonic flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1983., 1983), by Karl Gottfried Guderley, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
• A survey of transition research at AEDC (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1977., 1977), by Jack D. Whitfield, N. Sam Dougherty, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• Energy-based design methodology for air vehicle systems : aerodynamic correlation study (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2005., 2005), by R. S. Figliola, Clemson University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by John C. Adams, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Computational methods for problems in aerodynamics using parallel and vector architecture (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1990., 1990), by David Gottlieb, Brown University. Division of Applied Mathematics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Turbulence modeling (Ithaca, New York : Cornell University, Sibley School of Mechanical and Aerospace Engineering, 1994., 1994), by John L. Lumley, Sibley School of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Two-dimensional turbulent boundary layer separation on a flat plate with ramp at freestream Mach numbers of 3.7 and 6.3 in supersonic and hypersonic flow (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, 1975., 1975), by V. Zakkay, Aerospace Research Laboratories (U.S.), and New York University. Aerospace and Energetics Laboratory (page images at HathiTrust)
• Stability of a pair of stationary vortices in the leeward side of a cylinder in a potential flowfield (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), by Shiva N. Singh, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Kentucky. Department of Mechanical Engineering (page images at HathiTrust)
• Measurement and analysis of the external unsteady pressures on the airborne laser laboratory (Kirtland Air Force Base, New Mexico : Air Force Weapons Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Leonard J. Otten and United States. Air Force. Air Force Weapons Laboratory (page images at HathiTrust)
• Numerical study of separated turbulent flows (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Systems Command, 1974., 1974), by David C. Wilcox, Aerospace Research Laboratories (U.S.), and United States. National Technical Information Service (page images at HathiTrust)
• Subsonic flow of hot gas through a highly cooled constant-area channel (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), by Harold Mirels, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1972., 1972), by George F. Widhopf, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• On the viscosity of dissociated air (Buffalo, New York : Cornell University, Cornell Aeronautical Laboratory, 1961., 1961), by F. K. Moore, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Description and capabilities of the aeroballistic research facility (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Gunsm Rockets, and Explosives Division, Air Force Systems Command, United States Air Force, 1978., 1978), by G. L. Winchenback, Judith Sullivan Kleist, D. G. Galanos, Billy Lucas, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)
• Holographic interferometry measurements of subsonic turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), by D. W. Sinclair, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• Annual report including Technical reports. (U.S. Govt. Print. Off., 1915), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Modification and validation of conceptual design aerodynamic prediction method HASC95 with VTXCHN (National Aeronautics and Space Administration, 1996), by Alan E. Albright, Martin C. Hegedus, Charles J. Dixon, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code (National Aeronautics and Space Administration, Langley Research Center ;, 1995), by Tim A. Kinard, Pradeep Raj, Brenda W. Harris, and Langley Research Center (page images at HathiTrust)
• Effect of the acceleration of enlongated bodies of revolution upon the resistance in a compressible flow (NACA, 1949), by F. I. Frankl and Langley Aeronautical Laboratory (page images at HathiTrust)
• Collected works of K.E. Tsiolkovskiy. Volume III, Dirigibles (National Aeronautics and Space Administration, 1965), by K. T͡Siolkovskiĭ, A. A. Blagonravov, United States National Aeronautics and Space Administration, and Faraday Translations (page images at HathiTrust)
• Stability of systems containing a heat source - the Rayleigh criterion (National Advisory Committee for Aeronautics, 1956), by Boa-Teh Chu and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)

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