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Aerodynamics

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Filed under: Aerodynamics

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)
Scientific fairing of veneer fuselages., by United States. Bureau of Aircraft Production (page images at HathiTrust)
Aerodynamics of deflected slipstreams. (Buffalo, Cornell Aeronautical Laboratory, 1961-), by Alexander Sowyrda (page images at HathiTrust; US access only)
Aerodynamics; constituting the first volume of a complete work on aerial flight. (London, Constable, 1911), by F. W. Lanchester (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. / (London : Constable, 1918), by F. W. Lanchester (page images at HathiTrust)
An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect / (Washington, D.C. : National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Ralph L. Schacht, Arthur W. Goldstein, Richard R. Cullom, and Lewis Research Center (page images at HathiTrust)
The wind-induced loads on a dynamically scaled model of a large missile in launching position / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Donald A. Buell, George C. Kenyon, and Ames Research Center (page images at HathiTrust)
Force, moment, and flow-field characteristics of two wing-body-nacelle combinations at Mach numbers 2 and 3 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Thomas G. Gainer and Langley Research Center (page images at HathiTrust)
Transonic flutter investigation of models of proposed horizontal tails for the X-15 airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Lou S. Young and Langley Research Center (page images at HathiTrust)
Transonic flutter investigation of models of the X-15 airplane horizontal tail / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Lou S. Young, Samuel R. Bland, 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington : 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)
Introduction to aerodynamics of a compressible fluid, (New York Wiley, [1948, c1947]), by H. W. Liepmann and Allen E. jt Puckett (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)
Applied aeronautics, (Chicago : The Joseph G. Branch Pub. Co., [1943]), by Joseph G. Branch (page images at HathiTrust; US access only)
Systems identification using a modified Newton-Raphson method : A Fortran program / (Washington, D.C. : U.S. National Aeronautics and Space Administratration, 1972), by Lawrence W. Taylor and Kenneth W. Iliff (page images at HathiTrust)
Light aircraft lift, drag, and moment prediction : a review and analysis / (Washington, D.C. : National Aeronautics and Space Administration, 1975), by Frederick O. Smetana, Langley Research Center, and North Carolina State University (page images at HathiTrust)
Aerodynamics / (New York : The Macmillan Company, 1944), by Leslie Rendall Parkinson (page images at HathiTrust)
Nova experimenta physico-mechanica de vi aeris elastica et ejusdem effectibus, facta maximam partem in nova machina pneumatica ... / (Genevae : apud Samuelem de Tournes, 1680), by Robert Boyle, ant. pos. BHI BH MED 2579 Real Colegio de Cirugía de San Carlos (Madrid), and Samuel de Tournes (page images at HathiTrust)
Experimentorum novorum physico-mechanicorum continuatio secunda. In qua experimenta varia tum in aere compresso, tum in factitio, instituta, circa ignem, animalia, &c. ... / (Coloniae Allobrogum : apud Samuelem de Tournes, 1686), by Robert Boyle and Samuel de Tournes (page images at HathiTrust)
Oscillatory aerodynamic loads on low-aspect-ratio wings in subsonic flow. ([Boston : s. n.], 1955-), by Massachusetts Institute of Technology. Aerolastic and Structures Research (page images at HathiTrust; US access only)
Flight-velocity, (Hamburg, Boysen & Maasch; New York, Spon & Chaberlain; [etc., etc.], 1906), by Arnold Samuelson (page images at HathiTrust; US access only)
Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Robert S. Swanson, E. LaVerne Priddy, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
A method for studying the hunting oscillations of an airplane with a simple type of automatic control / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Robert T. Jones, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Neal Tetervin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Static-pressure error of an airspeed installation on an airplane in high-speed dives and pull-outs / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by John A. Zalovcik, Clotaire Wood, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Hinge moments of sealed-internal-balance arrangements for control surfaces. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Jack Fischel, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Carl F. Schueller, H. Kurt Strass, Peter F. Korycinski, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The theory of propellers. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Theodore Theodorsen, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of wing modifications on the longitudinal stability of a tailless all-wing airplane model / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Charles L. Seacord, Herman O. Ankenbruck, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Experimental determination of the effect of negative dihedral on lateral stability and control characteristics at high lift coefficients / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Marion O. McKinney, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryansky, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Paul Kuhn, Simon H. Diskin, John E. Duberg, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Tests of a stress-carrying door in compression / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by Robert Gottlieb, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel vibration tests of a four-blade single-rotating pusher propeller / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Mason F. Miller, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Tests of a stress-carrying door in shear / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by Robert Gottlieb, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Extended tables of stiffness and carry-over factor for structural members under axial load / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Eugene E. Lundquist, W. D. Kroll, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Investigation of methods of supporting single-thickness specimens in a fixture for determination of compressive stress-strain curves / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Joseph N. Kotanchik, Robert A. Weinberger, Walter Woods, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Data for design of entrance vanes from two-dimensional tests of airfoils in cascade / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Charles M. Zimmey, Viola M. Lappi, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of normal pressure on the critical shear stress of curved sheet / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Norman Rafel, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Robert T. Jones, Harry Greenberg, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Determination of desirable lengths of Z- and channel-section columns for local-instability tests / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by George J. Heimerl, J. Albert Roy, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by S. B. Batdorf, John C. Houbolt, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel investigation of control-surface characteristics. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by I. Elizabeth Garner, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Tensile tests of NACA and conventional machine-countersunk flush rivets / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Merven W. Mandel, Leonard M. Bartone, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Hinge moments of sealed-internal-balance arrangements for control surfaces. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harry E. Murray, Mary A. Erwin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by J. D. Bird, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high mach numbers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold F. Kleckner, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Hubert M. Drake, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
An approximate determination of the power required to move control surfaces as related to control-booster design / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel tests of dual-rotating propellers with systematic differences in number of blades, blade setting, and rotational speed of front and rear propellers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by W. H. Gray, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight investigation at high mach numbers of several methods of measuring static pressure on an airplane wing / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by John A. Zalovcik, Fred L. Daum, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of variation in diameter and pitch of rivets on compressive strength of panels with z-section stiffeners. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Norris F. Dow, William A. Hickman, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by S. B. Batdorf, Charles Libove, Manuel Stein, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Aerodynamic tests of an M-31 bomb in the 8-foot high-speed tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by Donald D. Baals, Norman F. Smith, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Supersonic-tunnel tests of projectiles in Germany and Italy / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Antonio Ferri, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The flow of a compressible fluid past a circular arc profile / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Carl Kaplan, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Aerodynamic tests of an AN-M-65-AZON 1000-pound radio-controlled bomb in the LMAL 16-foot high-speed tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by E. O. Pearson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Force tests of a 1/5-scale model of the type GB-5 controllable glide bomb / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Marvin Pitkin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight tests of the lateral control characteristics of an F6F-3 airplane equipped with spring-tab ailerons / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Walter C. Williams, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Calculation of stick forces for an elevator with a spring tab / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Harry Greenberg, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distribution / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Theodore Theodorsen, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Theoretical analysis of stationary potential flows and boundary layers at high speed = Theoretische untersuchungen über stationäre potentialströmungen und grenzschichten bei hohen geschwindigkeiten / (Washington, D.C. : NACA, 1948), by K. Oswatitsch, K. Wieghardt, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities / (Washington, D.C. : NACA, 1951), by L. G. Loĭt�si�anskiĭ and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Investigation of effect of sideslip on lateral stability characteristics. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Thomas A. Hollingworth, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by S. M. Harmon, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Paul E. Purser, Elizabeth G. McKinney, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Tests of a linked differential flap system designed to minimize the reduction in effective dihedral caused by power / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Marvin Pitkin, Robert O. Schade, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight measurements of the rudder control and sideslip characteristics of four vertical tail arrangements on the P-40 series airplanes / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by Harold I. Johnson, Joseph R. Vensel, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The use of geared spring tabs for elevator control / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by William H. Phillips, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel investigation of rounded horns and of guards on a horizontal tail surface / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Robert B. Liddell, Vernard E. Lockwood, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The conformal transformation of an airfoil into a straight line and its application to the inverse problem of airfoil theory / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by William Mutterperl, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
End-zone water injection as a means of suppressing knock in a spark-ignition engine / (Cleveland, OH : Aircraft Engine Research Laboratory, 1944), by Rinaldo J. Brun, Cearcy D. Miller, H. Lowell Olsen, United States. National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Robert W. Kamm, Frank S. Malvestuto, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold F. Kleckner, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
An electromagnetic-analogy method of solving lifting-surface-theory problems / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Robert S. Swanson, Stewart M. Crandall, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by John P. Campbell, John W. Paulson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Gerald G. Kayten, William Koven, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel investigation of an NACA 23021 airfoil with a 0.32-airfoil-chord double slotted flap / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Jack Fischel, John M. Riebe, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Investigation of effect of sideslip on lateral stability characteristics. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Thomas A. Hollingworth, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by E. O. Pearson, F. E. West, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel investigation of effects of a pusher propeller on lift, profile drag, pressure distribution, and boundary-layer transition of a flapped wing / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Carl A. Sandahl, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Investigation of effect of sideslip on lateral stability characteristics. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Leo F. Fehlner, Robert MacLachlan, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Note on compressibility effects on downwash at the tail at subcritical speeds / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Jack Norman Nielsen, Harold H. Sweberg, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight studies of the horizontal-tail loads experienced by a modern pursuit airplane in abrupt maneuvers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Langley Aeronautical Laboratory and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Charts of pressure, density, and temperature changes at an abrupt increase in cross-sectional area of flow of compressible air / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Upshur T. Joyner, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect on helicopter performance of modifications in profile-drag characteristics of rotor-blade airfoil sections / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by F. B. Gustafson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Myron J. Block, S. Katzoff, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Charts for determining propeller efficiency / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by John L. Crigler, Herbert W. Talkin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Spinning of large airplanes / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Oscar Seidman, United States. National Advisory Committee for Aeronautics, and Langley Air Force Base (Va.). Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of lateral shift of center of gravity on rudder deflection required for trim / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by W. H. Phillips, P. A. Hunter, H. L. Crane, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Stability in a body stabilized by fins and suspended from an airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by William H. Phillips, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Determination of the stability and control characteristics of a tailless all-wing airplane model with sweepback in the Langley free-flight tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by John P. Campbell, Charles L. Seacord, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Maximum rates of control motion obtained from ground tests / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by De E. Beeler, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by John A. Zalovcik, Fred L. Daum, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effects of heat-capacity lag in gas dynamics / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Arthur Kantrowitz, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by J. D. Bird, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel investigation of a rectangular NACA 2212 airfoil with semispan ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Thomas A. Toll, Margaret F. Ivey, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Application of spring tabs to elevator controls / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by William H. Phillips, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
A simple method for estimating terminal velocity including effect of compressibility on drag / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Ralph P. Bielat, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The theory of propellers. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Theodore Theodorsen, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of compressibility on the pressures and forces acting on a modified NACA 65,3-019 airfoil having a 0.20-chord flap / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by W. F. Lindsey, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Milton D. Humphreys, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Resistance tests of models of three flying-boat hulls with a length-beam ration of 10.5 / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Jerold M. Bidwell, David M. Goldenbaum, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22 1/2À / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Wilbur L. Mayo, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by W. F. Lindsey, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
An automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane / (Langley Field, VA : 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 / (Washington, D.C. : NACA, 1952), by J. Pretsch and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Heat transmission in the boundary layer / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1949), by August Wilhelm Quick, K. Schröder, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
On rotational conical flow / (Washington, D.C. : NACA, 1952), by Carlo Ferrari and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Concerning the flow about ring-shaped cowlings. (Washington, D.C. : 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. (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1953), by K. Wieghardt, W. Tillmann, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Steady vibrations of wing of circular plan form, and, theory of wing of circular plan form / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1954), by I. T. Aladyev and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Lift on a bent, flat plate / (Washington, D.C. : NACA, 1955), by F. Keune and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Air admixture to exhaust jets / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1952), by Itiro Tani and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Concerning the flow about ring-shaped cowlings. (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1949), by J. Meixner and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
On stability and turbulence of fluid flows / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1952), by Robert Betchov, W. Welling, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Concerning the flow about ring-shaped cowlings. (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1947), by K. I. Shelkin and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Infinitesimal conical supersonic flow / (Washington, D.C. : NACA, 1947), by Adolf Busemann and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Calculation of turbulent expansion processes / (Washington, D.C. : NACA, 1945), by Walter Tollmien and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Lecture series "boundary layer theory." (Washington, D.C. : NACA, 1949), by H. Schlichting and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The plane problem of the flapping wing / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1947), by Karl Marguerre and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The elliptic wing based on the potential theory / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1949), by H. Schlichting and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The flow of gases in narrow channels / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1949), by D. Küchemann and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
On the theory of the Laval nozzle / (Washington, D.C. : NACA, 1949), by S. V. Falkovich and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The effect of artificial aging on the tensile properties of alclad 24S-T and 24S-T aluminum alloy / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Joseph N. Kotanchik, George W. Zender, Walter Woods, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Compression shocks in two-dimensional gas flows / (Washington, D.C. : NACA, 1949), by Adolf Busemann, J. Vanier, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boat / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Douglas A. King, Newton A. Mas, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Carl F. Schueller, Peter F. Korycinski, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Nonstationary gas flow in thin pipes of variable cross section / (Washington, D.C. : NACA, 1948), by G. Guderley, Dave Feingold, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
A study of the effects of radii of gyration and altitude on aileron effectiveness at high speed / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Leo F. Fehlner, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Marvin Pitkin, Charles V. Bennett, John W. Draper, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The belt method for measuring pressure distribution / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Blake W. Corson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
NACA mach number warning device for use in flight / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Jerry Goodman, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Comparison between calculated and measured loads on wing and horizontal tail in pull-up maneuvers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Cloyce E. Matheny, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight investigation of NACA Ds cowlings on the XP-42 airplane. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by J. Ford Johnston, T. J. Voglewede, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Evan H. Schuette, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
A flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Walter C. Williams, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Comparison of tightness of 78À machine-countersunk rivets driven in holes prepared with 78À and 82À countersinking tools / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by Robert Gottlieb, Merven W. Mandel, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The effect of initial displacement of the center support on the buckling of a column continuous over three supports / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1940), by Eugene E. Lundquist, Joseph N. Kotanchik, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Development of cowling for long-nose air-cooled engine in the NACA full-scale wind tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1941), by Abe Silverstein, Eugene R. Guryansky, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by W. C. Williams, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The NACA impact basin and water landing tests of a float model at various velocities and weights / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Sidney A. Batterson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Some notes on the determination of the stick-free neutral point from wind-tunnel data / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Marvin Schuldenfrei, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Experimental study of flow past turbine blades / (Washington, D.C. : NACA, 1949), by E. Eckert, K. von Vietinghoff-Scheel, J. Vanier, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight investigation of wing-gun fairings on a fighter type airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1941), by J. M. Nissen, M. D. White, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Column and plate compressive strengths of aircraft structural materials 24S-T aluminum-alloy sheet / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Eugene E. Lundquist, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Gas motion in a local supersonic region and conditions of potential-flow breakdown / (Washington, D.C. : NACA, 1949), by A. A. Nikol§skiĭ, G. I. Taganov, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The determination of effective column length from strain measurements / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Evan H. Schuette, J. Albert Roy, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy method / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by S. Katzoff, Robert S. Finn, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flow of gas through turbine lattices / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1956), by M. E. Deĭch, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Finite span wings in compressible flow / (Washington, D.C. : NACA, 1956), by E. A. Krasil§shchikova and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Remark on the theory of lifting surfaces / (Washington, D.C. : NACA, 1956), by Aldo Muggia and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by John P. Campbell, Thomas A. Hollingworth, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Apparatus for measurements of time and space correlation / (Washington, D.C. : NACA, 1955), by Alexandre Favre, R. Dumas, J. Gaviglio, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flat plate cascades at supersonic speed / (Washington, D.C. : NACA, 1956), by Rashad M. El Badrawy and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Emergency measures for increasing the range of fighter airplanes / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Robert T. Jones, Joseph W. Wetmore, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth / (Washington, D.C. : NACA, 1954), by William K. Koffel, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Theoretical distribution of load over a swept-back wing / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by Doris Cohen, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures / (Washington, D.C. : NACA, 1953), by Warren H. Lowdermilk, John N. B. Livingood, Walter F. Weiland, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Experiments on drag of revolving disks, cylinders and streamline rods at high speeds / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Theodore Theodorsen, Arthur A. Regier, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Kinetic treatment of the nucleation in supersaturated vapors / (Washington, D.C. : NACA, 1954), by R. Becker, Werner Döring, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Some measurements of time and space correlation in wind tunnel / (Washington, D.C. : NACA, 1955), by Alexandre Favre, R. Dumas, J. Gaviglio, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Supersaturation in the spontaneous formation of nuclei in water vapor / (Washington, D.C. : NACA, 1953), by Adolf Sander, Gerhard Damköhler, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
General solutions of optimum problems in nonstationary flight / (Washington, D.C. : NACA, 1955), by Angelo Miele, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
On the gas dynamics of a rotating impeller / (Washington, D.C. : NACA, 1956), by Adolf Busemann and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
A method of quadrature for calculation of the laminar and turbulent boundary layer in case of plane and rotationally symmetrical flow / (Washington, D.C. : NACA, 1955), by Erich Truckenbrodt and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The theory of propellers. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Theodore 31262081065491Theodorsen and Langley Aeronautical Laboratory (page images at HathiTrust)
Analysis of available data on the effectiveness of ailerons without exposed overhang balance / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Robert S. Swanson, Stewart M. Crandall, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Column and plate compressive strengths of aircraft structural materials extruded 75S-T aluminum-alloy / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by George J. Heimerl, J. Albert Roy, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wind-tunnel investigation of control-surface characteristics. (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by John M. Riebe, Oleta Church, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Climb and high-speed tests of a Curtiss no. 714-1C2-12 four-blade propeller on the Republic P-47C airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by A. W. Vogeley, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by H. A. Pearson, William S. Aiken, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Analysis of vertical-tail loads in rolling pull-out maneuvers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Robert R. Gilruth, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The relation between spanwise variations in the critical mach number and spanwise load distributions / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Richard T. Whitcomb, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Marion O. McKinney, Bernard Maggin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight / (Washington, D.C. : NACA, 1953), by Norman M. McFadden, Harry A. James, John L. McCloud, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
A study of the flow over a 45À sweptback wing -fuselage combination at transonic Mach numbers / (Washington, D.C. : NACA, 1952), by Richard T. Whitcomb, Thomas C. Kelly, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Tire friction coefficients and their relation to ground-run distance in landing / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1942), by F. B. Gustafson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates / (Washington, D.C. : NACA, 1954), by Eldon W. Sams, Walter F. Weiland, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
A summary of available knowledge concerning skin friction and heat transfer and its application to the design of high-speed missiles / (Washington, D.C. : NACA, 1951), by Morris W. Rubesin, Steven A. Varga, Charles B. Rumsey, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag / (Washington, D.C. : NACA, 1957), by Robert L. Nelson, Clement J. Welsh, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Survey of advantages and problems associated with transpiration cooling and film cooling of gas-turbine blades / (Washington, D.C. : NACA, 1951), by E. R. G. Eckert, Jack B. Esgar, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Experimental pressure distributions over two wing-body combinations at Mach number 1.9 / (Washington, D.C. : NACA, 1951), by Barry Moskowitz, Stephen H. Maslen, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
An approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow / (Washington, D.C. : NACA, 1949), by Coleman duP. Donaldson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Qualitative measurements of the effective heats of ablation of several materials in supersonic air jets at stagnation temperatures up to 11,000À F / (Washington, D.C. : NACA, 1958), by Bernard Rashis, Russell N. Hopko, William G. Witte, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number of 1.5 / (Washington, D.C. : NACA, 1947), by Dean R. Chapman, Edward W. Perkins, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane / (Washington, D.C. : NACA, 1958), by Bennie W. Cocke, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Exploratory investigation of transpiration cooling of a 40À double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295À to 2,910À F / (Washington, D.C. : NACA, 1957), by Bernard Rashis, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations / (Washington, D.C. : NACA, 1955), by Harry W. Carlson, John P. Gapcynski, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310À and 3,500À R on a magnesium fin with several leading-edge modifications / (Washington, D.C. : NACA, 1957), by W. M. Bland, Walter E. Bressette, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Temperature recovery factors on a slender 12À cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45À / (Washington, D.C. : NACA, 1955), by John O. Reller, Frank M. Hamaker, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
A method for simulating the atmospheric entry of long-range ballistic missiles / (Washington, D.C. : NACA, 1955), by A. J. Eggers, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
Preliminary survey of possible cooling methods for hypersonic aircraft / (Washington, D.C. : NACA, 1958), by Jack B. Esgar, Francis S. Stepka, Robert O. Hickel, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number / (Washington, D.C. : NACA, 1957), by Virgil E. Johnson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface / (Washington, D.C. : NACA, 1957), by Virgil E. Johnson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Note on the importance of imperfect-gas effects and variation of heat capacities on the isentropic flow of gases / (Washington, D.C. : NACA, 1948), by Coleman duP. Donaldson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Wire cloth as porous material for transpiration-cooled walls / (Washington, D.C. : NACA, 1951), by E. R. G. Eckert, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Procedure for calculating turbine blade temperatures and comparison of calculated with observed values for two stationary air-cooled blades / (Washington, D.C. : NACA, 1952), by W. Byron Brown, Hadley T. Richards, Henry O. Slone, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Langley full-scale-tunnel tests of the custer channel wing airplane / (Washington, D.C. : NACA, 1953), by Jerome Pasamanick, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Aircraft configurations developing high lift-drag ratios at high supersonic speeds / (Washington, D.C. : NACA, 1956), by A. J. Eggers, Clarence A. Syvertson, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
Frequency of occurrence of atmospheric gusts and of related loads on airplane structures / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Richard V. Rhode, Philip Donely, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Formation of a vortex at the edge of a plate / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1956), by G. M. Corcos, H. W. Liepmann, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
On the spectrum of natural oscillations of two-dimensional laminar flows / (Washington, D.C. : NACA, 1957), by D. Grohne and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Concerning the flow about ring-shaped cowlings. (Washington : 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 / (Washington, D.C. : NACA, 1948), by A. Weigand and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
On the statistical theory of turbulence / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1952), by B. Göthert and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Boundary layer / (Washington : 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 / (Washington, D.C. : NACA, 1952), by Lorenzo Poggi and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The elasto-plastic stability of plates / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : NACA, 1956), by A. E. Donov and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Autogenous welding in airplane construction / (Washington, D.C. : NACA, 1929), by Ludwig Kuchel 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 / (Washington, D.C. : NACA, 1952), by E. Sponder and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The aerodynamic analysis of single and multiple vehicles [entering and traveling in open tunnels] / (Washington : Dept. of Transportation, Federal Railroad Administration, Office of Research, Development, and Demonstration ; Springfield, Va. : For sale by the National Technical Information Service, 1975), 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 / (Washington, DC : U.S. Department of Transportation, Federal Aviation Administration, Systems Research and Development Service ; Springfield, Va. : National Technical Information Service [distributor, 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)
Meteorology and aeronautics. (Washington, Govt. Printing Office., 1917), by United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Environmental effects on space shuttle reusable surface insulation coated with reaction cured glass / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by George C. Greene and Langley Research Center (page images at HathiTrust)
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90/̊ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Three-dimensional flow of ideal gas past smooth bodies / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by Konstantin Ivanovich Babenko (page images at HathiTrust)
A laminar theory of the flow through a turbo-machine. (Troy, N.Y., 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, ([Washington, U. S. Govt. print. off.], 1939), by Eastman Nixon Jacobs and Ira Herbert Abbot (page images at HathiTrust; US access only)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature. (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1957-), by Zbiginew Krzywoblocki (page images at HathiTrust; US access only)
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 / (London : H.M.S.O., 1910), by G. Greenhill (page images at HathiTrust)
Theory of a stream line past a curved wings, (London : H. M. Stationery off., Sir J. Causton and sons, limited [printers], 1916), by G. Greenhill (page images at HathiTrust)
Structural Dynamics Division research and technology accomplishments for FY 1988 and plans for FY 1989. ([Hampton, Va. : Langley Research Center, 1989]), by James E. Gardner, Langley Research Center. Structures and Dynamics Division, and Langley Research Center (page images at HathiTrust)
On the nonlinear three-dimensional instability of Stokes layers and other shear layers to pairs of oblique waves / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1993), by Xuesong Wu, Stephen J. Cowley, Sang Soo Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster / (Washington D.C. : National Aeronautics and Space Administration, 1960), by Albin O. Pearson and Langley Research Center (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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Bruce G. Powers, David A. Kier, and Flight Research Center (U.S.) (page images at HathiTrust)
Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel / (Washington [D.C.] : NASA, 1963), by Rodger L. Naeseth, Thomas G. Gainer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A theoretical method for the analysis and design of axisymmetric bodies / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by T. D. Beatty, Langley Research Center, and McDonnell Douglas Corporation (page images at HathiTrust)
Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1971), by Alan D. Levin, Ronald C. Smith, 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 : I. Subsonic / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1971), by Ronald C. Smith, Alan D. Levin, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Fixed-base simulator study of the effect of time delays in visual cues on pilot tracking performance / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by M. J. Queijo, Donald R. Riley, and Langley Research Center (page images at HathiTrust)
Dynamical mechanisms producing large-scale transport of atmospheric trace substances / (Monterey, California : Naval Postgraduate School, 1970), by J. D. Mahlman and Naval Postgraduate School (U.S.) (page images at HathiTrust)
Flow-separation patterns on symmetric forebodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986), by Earl R. Keener (page images at HathiTrust)
Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds / (Washington, [DC] : 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 / (Washington, [DC] : 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)
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 / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Bernard Spencer and United States National Aeronautics and Space Administration (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 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Robert G. Dorsch, Murray Dryer, Harrison Allen, and Lewis Research Center (page images at HathiTrust)
Weak-wave analysis of shock interaction with a slipstream / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988), by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers / ([Washington, DC] : National Aeronautics and Space Administration, 1986), by John C. org. AVSCOM. Wilson, Henry L. org. AVSCOM. 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)
NASA Aerodynamics Program : annual report 1990 / ([Washington, D.C.] : 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)
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 / (Washington [D.C.] : 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 / (Washington [D.C.] : 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)
Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by James L. Bettner, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
Theoretical study of ducted fan performance / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by M. R. Mendenhall, Selden B. Spangler, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
A computer program for the prediction of ducted fan performance / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by M. R. Mendenhall, Selden B. Spangler, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
Numerical results for the diffraction of a normal shock wave by a sphere and for the subsequent transient flow / (Washington : National Aeronautics and Space Administration, 1967), by Richard W. Barnwell (page images at HathiTrust)
A study of the simulation of flow with free-stream Mach number 1 in a choked wind tunnel / (Washington, DC : U.S. G.P.O., 1960), by John R. Spreiter, B. Jeanne Hyett, Donald W. Smith, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Analytic study of induced pressure on long bodies of revolution with varying nose bluntness at hypersonic speeds / (Washington, DC : U.S. G.P.O., 1960), by Vernon Van Hise, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service], 1972), by Robert W. Rainey and Langley Research Center (page images at HathiTrust)
Subsonic annular wing theory with application to flow about nacelles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Michael J. Mann 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 / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
Relative operating capabilities of selected electric-arc reentry environment simulators / ([Washington, D.C.] 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)
Geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment / (Washington : National Aeronautics and Space Administration ; [Springfield, Va. : Distributed by National Technical Information Service], 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)
Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, VA] : National Technical Information Service, distributor, 1963), by H. Jullian Allen, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
A rapid numerical solution to subsonic flow over planar and axisymmetric profiles at an angle of attack of 0 ̊/ (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service],), by Vincent R. Mascitti and Langley Research Center (page images at HathiTrust)
Panel methods : an introduction / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Larry L. Erickson and Ames Research Center (page images at HathiTrust)
Detailed flow-field measurements over a 75 ̊swept delta wing / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Scott O. Kjelgaard, William L. Sellers, and Langley Research Center (page images at HathiTrust)
Flow-induced resonance of screen-covered cavities / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Paul T. Soderman and Ames Research Center (page images at HathiTrust)
Aeroacoustic and aerodynamic applications of the theory of nonequilibrium thermodynamics / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by W. Clifton Horne, Krishnamurty Karamcheti, Charles A. Smith, and Ames Research Center (page images at HathiTrust)
Ground effects on the low-speed aerodynamics of a powered, generic hypersonic configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by W. Kyle Anderson and Langley Research Center (page images at HathiTrust)
Subsonic sting interference on the aerodynamic characteristics of a family of slanted-base ogive-cylinders / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Evaluation of the gust-alleviation characteristics and handling qualities of a free-wing aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
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 / (Washington, D.C., : 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)
Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1968), by Odell A. Morris, Robert J. Mack, 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 / (Washington, D.C. : 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)
Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Delma C. Freeman, Langley Research Center, and United States National Aeronautics and Space Administration (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 ̊/ (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Leland H. Jorgensen and Ames Research Center (page images at HathiTrust)
Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 / (Washington, D.C. : 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)
Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1968), by Richard J. Margason, Garl L. Gentry, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Spherical balloon response to three-dimensional time-dependent flows / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by George H. Fichtl and George C. Marshall Space Flight Center (page images at HathiTrust)
Performance comparisons of high mach number compressor rotor blading / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
A study of NACA and NASA published information of pertinence in the design of light aircraft. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 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 / (Washington, D.C. : 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)
An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by F. A. Woodward, Langley Research Center, and Aerophysics Research Corporation (page images at HathiTrust)
Effects of a pointed nose on spin characteristics of a fighter airplane model including correlation with theoretical calculations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 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)
An experimental investigation of the airflow over a cavity with antiresonance devices / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1971), by Donald A. Buell, Ames Research Center, and United States National Aeronautics and Space Administration (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 (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Paul B. Gooderum, Dennis M. Bushnell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by James L. Thomas, Delwin R. Croom, Danny R. Hoad, and Langley Research Center (page images at HathiTrust)
Development and application of a local linearization algorithm for the integration of quaternion rate equations in real-time flight simulation problems (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Lawrence E. Barker, Louise H. Williams, Roland L. Bowles, United States National Aeronautics and Space Administration, and Langley 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 (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Harry A. Verstynen, Dominick Andrisani, United States National Aeronautics and Space Administration, and Langley 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, ([Washington, U.S. G.P.O.], 1959), by Virgil S. Ritchie (page images at HathiTrust)
Slender-body theory based on approximate solution of the transonic flow equation / (Washington, DC : U.S. G.P.O., 1959), by John R. Spreiter, Alberta Y. Alksne, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Nearly circular transfer trajectories for descending satellites / (Washington, DC : 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)
Stability of a horizontal fluid layer with unsteady heating from below and time-dependent body force / (Washington, DC : U.S. G.P.O., 1959), by Arthur W. Goldstein, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
Stagnation-point shielding by melting and vaporization / (Washington, DC : U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Vernard E. Lockwood, Aniello Matarazzo, and Langley Research Center (page images at HathiTrust)
Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight / (Washington [D.C.] : 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)
Experimental and theoretical studies of the effects of camber and twist on the aerodynamic characteristics of parawings having normal aspect ratios of 3 and 6 / (Washington [D.C.] : NASA, 1963), by Edward C. Polhamus, Rodger L. Naeseth, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Computed lateral rate and acceleration power spectral response of conventional and STOL airplanes to atmospheric turbulence / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements / (Washington, D.C. : 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)
A comparison of the performance of four side-mounted inlets over a Mach number range of 0.88 to 2.2 and angles of attack to 14° / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Leroy L. Presley, William P. Peterson, and Ames 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° / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by John E. Grimaud and Langley Research Center (page images at HathiTrust)
Recombination of carbon monoxide and atomic oxygen at high temperatures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Theodore A. Brabbs, Frank E. Belles, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Aerodonetics : constituting the second volume of a complete work on aerial fight / (London : Constable, 1917), by F. W. Lanchester (page images at HathiTrust; US access only)
Development of an efficient procedure for calculating the aerodynamic effects of planform variation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by J. E. Mercer, E. W. Geller, Flow Research Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Harry W. Carlson, Kenneth B. Walkley, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
An analysis of the crossover between local and massive separation on airfoils / (Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1987), by M. Burnett, J. E. Carter, and Langley Research Center (page images at HathiTrust)
U.S.A. wing and propeller sections and biplane wing combinations., by United States. Bureau of Aircraft Production (page images at HathiTrust)
Lautaret engine tests., by United States. Bureau of Aircraft Production (page images at HathiTrust)
Section technique aeronautique radiator tests, by United States. Bureau of Aircraft Production (page images at HathiTrust)
Théorie générale des régimes de l'aéroplane. (Paris, 1913), by Georges de Bothezat (page images at HathiTrust; US access only)
Theory of flight / (Washington, D.C. : GPO, 1941), by United States War Department (page images at HathiTrust)
Experimentorum novorum physico-mechanicorum continuatio secunda : in qua experimenta varia tum in aere compresso, tum in factitio, instituta, circa ignem, animalia, &c. ... / (Genevae : apud Samuelem de Tournes, 1682), by Robert Boyle, Samuel de Tournes, and ant. pos. BHI BH DER 12634 Universidad Complutense (Alcalá de Henares) (page images at HathiTrust)
Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by William J. Alford, William P. Handerson, Arvo A. Luoma, and Langley Research Center (page images at HathiTrust)
Solution of complex nonlinear problems by a generalized application of the method of base and comparison solutions with applications to aerodynamics problems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Raymond L. Barger, Langley Research Center, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Airplane aerodynamics / (New York : Pitman Pub. Corp., c1957), by Daniel O. Dommasch (page images at HathiTrust; US access only)
A Review of near-wall Reynolds-stress closures / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Ronald M. C. So, Langley Research Center, and Arizona State University. College of Engineering and Applied Sciences (page images at HathiTrust)
Aerodonetics : constituting the second volume of a complete work on aerial flight / (New York : Van Nostrand, 1909), by F. W. Lanchester (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 / ([Washington] : 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)
Die Flugmaschine : des dynamischen Flugprincipes in ihrer Ausfuhrung und Verwendung / (Wien ; Leipzig : W. Braumüller, 1898), by Eduard Mánfai (page images at HathiTrust; US access only)
Solution du problème de la locomotion aérienne; aperçu général & sommaire, avec 21 figures à l'appui, (Paris, Carilian-Gœury et V. Dalmont; [etc., etc.], 1853), by Michel Loup (page images at HathiTrust)
The laws of Avanzini : laws of planes moving at an angle in air and water / (London : E. & F.N. Spon ; New York : Spon & Chamberlain, 1912), by Richard De Villamil and Giugeppe Avanzini (page images at HathiTrust)
The Coanda effect / ([Oak Ridge, Tenn.] : U.S. Atomic Energy Commission, Technical Information Service, 1959), by U.S. Atomic Energy Commission, Albert Metral, and Friedrich Zerner (page images at HathiTrust)
Propagation of density disturbances in air-water flow / (Evanston, Ill., 1965), by George Peter Nassos (page images at HathiTrust)
The mechanical principles of the aeroplane, (New York, Macmillan, 1921), by Selig Brodetsky (page images at HathiTrust)
Effects of Reynolds number and body corner radius on aerodynamic characteristics of a space shuttle-type vehicle at subsonic Mach numbers / (Washington, D.C. : 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)
Advanced technology airfoil research. (Washington, D.C. : National Aeronautics and Space Administration, 1979-), by NASA Conference on Advanced Technology Airfoil Research (1978 : Langley Research Center) (page images at HathiTrust)
Proceedings of the Circulation-Control Workshop 1986 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Circulation-Control Workshop (1986 : NASA Ames Research Center) and Jack Norman Nielsen (page images at HathiTrust)
Vortex-lattice utilization : a workshop held at Langley Research Center, Hampton, Virginia, on May 17-18, 1976 / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by National Technical Information Service, 1976), by Langley Research Center Vortex-Lattice Utilization Workshop and Langley Research Center (page images at HathiTrust)
Aerodynamic analyses requiring advanced computers : a conference held at Langley Research Center in Hampton, Virginia on March 4-6, 1975 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Office ; Springfield, Va. : for sale by the National Technical Information Service, 1975), by Langley Research Center (page images at HathiTrust)
Applied aerodynamics, (New York, [1919?]), by G. P. Thomson (page images at HathiTrust; US access only)
Prinzipien der Flugtechnik / (Rostock i.M. : C.J.E. Volckmann nachfolger (E. Wette), 1910), by Aladár Zsélyi (page images at HathiTrust; US access only)
Airplane design; aerodynamics. (New York, McGraw-Hill book company, inc., 1927), by Edward Pearson Warner (page images at HathiTrust)
Aerodyamics of the helicopter, (New York, Macmillan, [1952]), by Alfred Gessow (page images at HathiTrust)
Aérodynamique / (Paris : 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 (Leipzig, Veit & comp., 1911), by Adolf Lippmann (page images at HathiTrust; US access only)
L'air et la vitesse; vues nouvelles sur l'aviation; (Paris, Librairie aéronautique, 1919), by René Lorin (page images at HathiTrust; US access only)
The mechanics of the aeroplane : a study of the principles of flight. (London, New York [etc.] : Longmans, Green and co., 1917), by Emile Duchêne, T. O'B. Hubbard, and J. H. Ledeboer (page images at HathiTrust; US access only)
Aeronautics in theory and experiment, (London, E. Arnold, 1918), by William Lewis Cowley and H. Levy (page images at HathiTrust; US access only)
Essais sur la résistance de l'air et le calcul des aéroplanes, (Grenoble, Impr. A. Anselme, 1911), by Joseph Chovet (page images at HathiTrust; US access only)
La photographie du vent : etude photographique du champ aérodynamique. (Paris : Gauthier-Villars, 1911), by Auguste Lafay (page images at HathiTrust; US access only)
Graphische Berechnungs-Methoden : im Dienste der Naturwissenschaft und Technik / (Zürich-Selnau : Verlag Gebr. Leemann, 1910-1912), by Hans Mettler (page images at HathiTrust; US access only)
Über messung von dynamischem und statischen druck bewegter luft. (Munchen, Berlin, R. Oldenbourg, 1904), by Otto Krell (page images at HathiTrust; US access only)
Über die Lage des aerodynamischen Druckmittelpunktes an ebenen und gewölbten Flächen ... / (Kiel, Druck von Lüdtke & Martens, 1912), by Rudolf Benitt (page images at HathiTrust; US access only)
Gas dynamics tables for air. (New York : Dover Publications, [c1947]), by H. W. Emmons (page images at HathiTrust)
Experimental and theoretical studies of axisymmetric free jets / (Washington, DC : 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)
Variation in load factor factor experience of Fokker F27 and F28 operational acceleration exceedance data / (Washington, DC : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [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)
Homing performance comparison of selected airframe configurations using skid-to-turn and bank-to-turn steering policies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Royce D. Moore, George W. Lewis, George Kovich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Reduction of incremental load factor acceleration data to gust statistics / (Atlantic City International Airport, N.J. : FAA Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [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 / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [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 / (Atlantic City International Airport, N.J. : FAA Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [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)
Statistical loads data for Boeing 737-400 aircraft in commercial operations / (Washington, D.C.: Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1998]), by John Rustenburg, Daniel O. Tipps, Donal Skinn, University of Dayton. Research Institute, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
On the two-dimensional flow of air past a series of Rankine ovals, (Washington, Catholic University of America, 1932), by Laurence Ward Sheridan (page images at HathiTrust; US access only)
Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds / (Washington, D.C. : U.S. Government Printing Office, 1957), by Percy J. Bobbitt and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Chord-wise air load distribution : War Dept., Army Air Forces : Navy Dept., Bureau of Aeronautics : Dept. of Commerce, Civil Aeronautics ... / ([Washington?] : [U.S. Govt. Print. Off.?], 1942), by United States. Army-Navy-Civil Committee on Aircraft Design Criteria (page images at HathiTrust)
The drag of airplane wheels, wheel fairings and landing gears. (Washington, D.C. : National Advisory Committee for Aeronautics, [1934]), by David Biermann and William H. Herrnstein (page images at HathiTrust)
Electrical characteristics of spark generators for automotive ignition / (Washington, D.C. : National Advisory Committee for Aeronautics, 1926), by R. B. Brode, F. B. Silsbee, D. W. Randolph, and Langley Aeronautical Laboratory (page images at HathiTrust)
Recirculation principle for ground effect machine two-dimensional tests. ([Arlington, Va., Obtainable from Armed Services Technical Information Agency] illus., 27 cm), 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 ([Washington, 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)
Theoretical investigation of ducted propeller aerodynamics / (Farmingdale, NY : Republic Aviation, 1960), by Theodore Theodorsen (page images at HathiTrust)
NACA conference on some problems of aircraft operation; a compilation of the papers presented. ([Washington?, National Advisory Coimmittee for Aeronautics, 1950]), by Lewis Flight Propulsion Laboratory NACA Conference on Some Problems of Aircraft Operation and Lewis Research Center (page images at HathiTrust)
Demand bibliography : computational fluid dynamics / ([Alexandria, Va.] : Defense Technical Information Center, [1989]), by Defense Technical Information Center (U.S.) (page images at HathiTrust)
Thermal effects on static aeroelastic stability and control. (Wright-Patterson Air Force Base, O. : 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. (Washington, Distributed by United States Department of Commerce, Office of Technical Services, [1959?]), by I. V. Ostoslavskiĭ and I. V. Aerodinamika samoleta Ostoslavskiĭ (page images at HathiTrust)
La mécanique de l'aviation; (Paris, Librairie aéronautique, [1917]), by René Devillers (page images at HathiTrust; US access only)
Stability of the boundary layer; (Dayton, O., Air Material Command, Wright-Patterson Air Force Base, [1948]), by Peter Chiarulli and John Clinton Freeman (page images at HathiTrust)
Theoretical and experimental studies of airfoil characteristics in nonuniform sheared flow. ([Fort Eustis, U. S. Army Aviation Materiel Laboratories], 1965), by William Gordon Brady (page images at HathiTrust)
Tables of two-dimensional oscillating airfoil coefficients for rotary wings. (Buffalo, N.Y., Cornell Aeronautical Laboratory, Inc., 1955), by Robert G. Loewy (page images at HathiTrust)
Theoretical aerodynamics. (Ithaca, N.Y., 1951-), by William Rees Sears (page images at HathiTrust)
Einführung in die mechanik, mit einfachen beispielen aus der flugtechnik, (Berlin, J. Springer, 1917), by Th. Pöschl (page images at HathiTrust; US access only)
Mach number table (₋gc=1.4) with correction factors for real air ([Daingerfield, Tex., General Dynamics Pomona Division, 1963), by Ernest Carlton Kennedy and H. C. Kerr (page images at HathiTrust; US access only)
Simple aerodynamics and the airplane. (Washington, U. S. Govt. print. off., 1927), by United States. Army. Air Corps and Charles Norton Monteith (page images at HathiTrust)
Simplified theory of flight (New York, D. Van Nostrand company, inc., 1941), by Thomas Charles Gillmer and Herman Erich Nietsch (page images at HathiTrust)
Simple aerodynamics and the airplane, (New York, The Ronald Press company, [c1929]), by Charles Norton Monteith, Clifton Carroll Carter, and Edwin Eugene Aldrin (page images at HathiTrust)
Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows / ([Cambridge, Mass.] : 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)
A review of the physical and thermodynamic properties of boric oxide / (Washington, D.C. : NACA, 1957), by Paul C. Setze, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Physics of aerodynamic noise. ([Washington] 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)
Correlation of sonic-boom theory with wind-tunnel and flight measurements / (Washington, D.C. : 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)
Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planforms / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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 hypersonic transport configuration at Mach 6.86 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 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)
Longitudinal aerodynamic characteristics of a twin-turbofan subsonic transport with nacelles mounted under the wings / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Francis J. Capone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Linearized theory of stagnation region skin friction and mass transfer at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Kenneth K. Yoshikawa, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Comparison of methods in calculating frequencies of corner-supported rectangular plates / (Washington, D.C. : 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)
Measurements of boundary layer transition, separation and streamline direction on rotating blades / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
Aerodynamics of the model airplane /, by Franz Wilhelm Schmitz (page images at HathiTrust; US access only)
Airplane design; performance. (New York, London, McGraw-Hill, 1936-), by Edward Pearson Warner (page images at HathiTrust; US access only)
Effects of two probe antennas on aerodynamic characteristics of Apollo spacecraft at Mach 10.03 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Lawrence E. Putnam, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Empirical equation for turbulent forced-convection heat transfer for prandtl numbers from 0.001 to 1000 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Uwe H. VonGlahn and Lewis 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by Charles D. Trescot, Cuyler W. Brooks, Lawrence E. Putman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Tables of supersonic flow around cones of large yaw, (Cambridge, 1949), by Massachusetts Institute of Technology. Dept. of Electrical Engineering. Center of Analysis and Zdeněk Kopal (page images at HathiTrust; US access only)
Flight dynamics in moving air / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by I︠U︡riĭ Pavlovich Dobrolenskiĭ (page images at HathiTrust; US access only)
Theoretical prediction of the effects of vortex flows on the loading, forces, and moments of slender aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Supt. of Docs., U.S. G.P.O.], 1961), by J. Richard Spahr and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Interference effects of single and multiple round or slotted jets on a VTOL model in transition / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1964), by Raymond D. Vogler, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
Experimental stagnation-point velocity gradients and heat-transfer coefficients for a family of blunt bodies at Mach 8 and angles of attack / (Washington, D.C. : 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)
A 4-microsecond flashing light synchronized with framing of motion-picture cameras and its application in Schlieren photography / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and technical Information, Springfield, Va. 22151], 1970), by Walter F. Lindsey, Joseph Burlock, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Approximation for distribution of flow properties in the angle-of-attack plane of conical flows / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Joseph W. Cleary, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Theoretical pressure distributions over arbitrarily shaped periodic waves in subsonic compressible flow, and comparison with experiment, (Washington, 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)
Determination of inflated shape and inertial properties of an all-flexible parawing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Blair B. Gloss, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Langley hotshot tunnel operations with helium at Mach numbers in excess of 30 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Charles G. Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Aerodynamic and deployment characteristics of single-keel solid and single-keel slotted personnel parawings / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 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)
Dimple, spall and perforation characteristics of thin plates of nine materials under hypervelocity impact / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and technical Information, Springfield, Va. 22151], 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)
A finite-step method for calculation of theoretical load distributions for arbitrary lifting-surface arrangements at subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by James A. Blackwell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Investigation of isothermal, compressible flow across a rotating sealing dam. (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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)
External aerodynamics of the magnetosphere, ([Washington] 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)
The stagnation-point boundary layer with suction and injection in equilibrium dissociating air / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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 programed [sic] loads / (Washington, D.C. : 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)
Practical aerodynamics and the theory of the aeroplane. A résumé of the principles evolved by past experiments. (London, Aeronautics Office, [1909]), by Baden Fletcher Smyth Baden-Powell (page images at HathiTrust)
The unsteady flow field about a right circular cone in unsteady flight. ([Wright-Patterson Air Force Base, Ohio, 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 Dept (page images at HathiTrust)
Aerodynamics of the propeller (Wright-Patterson Air Force Base, Dayton, Ohio, Air Documents Division, Intelligence Dept., Air Material Command, 1948), by Fritz Weinig (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 expiermental data / (Hampton, Va. : Langley Research Center, Langley Station, [1962]), by William R. Wells and William O. Armstrong (page images at HathiTrust; US access only)
Aerodynamic forces on freight trains / (Washington : Dept. of Transportation, Federal Railroad Administration, Office of Freight Systems ; Springfield, Va. : for sale bythe National Technical Information Service, 1978-), by Prakash B. Joshi and United States. Federal Railroad Administration. Office of Freight Systems (page images at HathiTrust)
Der Flug : ein auf der Wirkung strahlenden Luftdrucks beruhender Vorgang / (Kreuznach : Jung & Co., 1908), by Emil Jacob (page images at HathiTrust; US access only)
Multigrid methods : proceedings of a symposium held at Ames Research Center, Moffett Field, California, October 21-22, 1981 (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Symposium on Multigrid Methods (1981 : Ames Research Center) (page images at HathiTrust)
Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Bosworth and Dryden Flight Research Facility (page images at HathiTrust)
Buffet characteristics of the F-8 supercritical wing airplane / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1982), by Judith J. Watson and Langley Research Center (page images at HathiTrust)
An introduction to the aerodynamics of the airplane (W. Lafayette, Ind., Rose Company, c1949), by H. Serbin (page images at HathiTrust; US access only)
Aerodynamics of the oscillating air-foil in compressible flow ... ([Wright Field, O. : U.S. Headquarters air materiel command, 1947-]), by Samuel Noah Karp, Herschel Weil, and Shien Siu Shu (page images at HathiTrust; US access only)
De la locomotion mécanique dans l'air et dans l'eau, (Paris, A. Bertrand, 1864), by Gustave Lambert (page images at HathiTrust)
Flight control system manuals. ([Hawthorne, Calif., The Division], 1952-1956), by Inc. Northrop Aircraft and United States. Navy Dept. Bureau of Aeronautics. 1n (page images at HathiTrust)
Leitfaden der Flugtechnik. (Berlin, J. Springer, 1913), by Siegmund Huppert (page images at HathiTrust; US access only)
Mass unbalance in a simplified autospin system / (Urbana, Ill. : 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)
Bulletin de l'institut aérodynamique de Koutchino. (St-Pétersbourg : R. Golicke & A. Willborg, 1906-1923), by Moskovskiī institut kosmicheskoī fiziki and Aėrodinamicheskīĭ institut v Kuchini︠e︡ (page images at HathiTrust; US access only)
A survey of computational aerodynamics in the United States / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1977), by Alfred Gessow and Dana J. Morris (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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
Experimental evaluation of nacelle-airframe interference forces and pressures at Mach numbers of 0.9 to 1.4 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Daniel P. Bencze, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Approximation concepts for numerical airfoil optimization / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Modeling interface motion of combustion (MIMOC) : a computer code for two-dimensional, unsteady turbulent combustion / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Ahmed F. Ghoniem, Antoni K. Oppenheim, Cecil J. Marek, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Richard E. Maine, Kenneth W. Iliff, Hugh L. Dryden Flight 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 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Investigations of simulated aircraft flight through thunderstorm outflows / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 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. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
A geometry package for generation of input data for a three-dimensional potenial-flow program / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Aerodynamics/ACEE ([Washington, D.C.?] : National Aeronautics and Space Administration : For sale by the Supt. of Docs., U.S. G.P.O., [1981?]), by United States National Aeronautics and Space Administration (page images at HathiTrust)
Numerical aerodynamic simulation. (Moffett Field, Calif. : Ames Research Center ; Washington, D.C. : National Aeronautics and Space Administration, Office of Aeronautics and Space Technology, [1987]), by Ames Research Center and United States. Office of Aeronautics and Space Technology (page images at HathiTrust)
Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 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 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
User's manual for interactive LINEAR : a FORTRAN program to derive linear aircraft models / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1988), by Robert F. Antoniewicz, Brian P. Patterson, Eugene L. Duke, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : for sale by the National Technical Information Service], 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)
Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Jimmy L. Pittman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
NASA aviation safety reporting system : fourth quarterly report, January 15, 1977 - April 14, 1977 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Information Service, 1977), by Ames Research Center, Aviation Safety Reporting System (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
Aerodynamic properties of a flat plate with cavity for optical-propagation studies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Sonic-boom wave-front shapes and curvatures associated with maneuvering flight / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Raymond L. Barger, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by H. Harris Hamilton, Randolph A. Graves, 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 / (Washington, D.C. : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
NASA aerodynamics program, annual report 1991 / (Washington, D.C. : NASA, Office of Management, Scientific and Technical Information Program, 1992), by Louis J. Williams and United States. Office of Aeronautics and Space Technology (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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream mach numbers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : for sale by the National Technical Information Service], 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)
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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Charles J. Trefny, Joseph W. Wasserbauer, and Lewis Research Center (page images at HathiTrust)
Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Robert W. Walters, Douglas L. Dwoyer, and Langley 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Information Service, 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)
A simple method for converting frequency-domain aerodynamics to the time domain / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1980), by E. H. Dowell and Langley Research Center (page images at HathiTrust)
Passive control of wing/store flutter / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
The compressible aerodynamics of rotating blades based on an acoustic formulation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service] , 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by William D. Beasley, William D. McGhee, and Langley Research Center (page images at HathiTrust)
Performance of low-pressure-ratio low-tip-speed fan stage with blade tip solidity of 0.65 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 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 / (Washington, D.C. : 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)
Performance with and with inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For Sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : for sale by the National Technical Information Service], 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
A smoke generator system for aerodynamic flight research / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989), by David M. Richwine, Gene V. Tracy, Robert E. Curry, and Dryden Flight Research Facility (page images at HathiTrust)
Water-tunnel investigation of concepts for alleviation of adverse inlet spillage interactions with external stores / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Dan H. Neuhart, Matthew N. Rhode, and Langley Research Center (page images at HathiTrust)
Experimental characterization of the effects of pneumatic tubing on unsteady pressure measurements / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990), by Stephen A. Whitmore and Dryden Flight Research Facility (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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Paul G. Fournier and Langley Research Center (page images at HathiTrust)
Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
VIBRA, an interactive computer program for steady-state vibration response analysis of linear damped structures / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Lynn M. Bowman 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Wind-tunnel investigation of an advanced general aviation canard configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Aerodynamic performance of 0.4066-scale model of JT8D refan stage / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Effects of vortex flaps on the low-speed aerodynamic characteristics of an arrow wing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Long P. Yip, Daniel G. Murri, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
The aerodynamic performance of several flow control devices for internal flow systems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 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)
Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Investigation of installation effects on single-engine convergent-divergent nozzles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Michael J. See, James V. Cozzolongo, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Surrogate-equation technique for simulation of steady inviscid flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Gary M. Johnson, Lewis Research Center, 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 / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Vorticity interaction effects on blunt bodies / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by E. Clay Anderson, David C. Wilcox, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Finite element analysis of low speed viscous and inviscid aerodynamic flows / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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) / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 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). (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
A generalized vortex lattlice method for subsonic and supersonic flow applications / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Luis R. Miranda, William M. Baker, Robert D. Elliott, Lockheed-California Company, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
DYLOFLEX modifications to FLEXSTAB. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979-), by Patrick D'Auria, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
An exploratory aerodynamic and structural investigation of all-flexible parawings / (Washington, D.C. : 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)
Application of the Bernoulli enthalpy concept to the study of vortex noise and jet impingment noise / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by B. Lakshminarayana, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Theodore A. Reyhner, Boeing Commercial Airplane Company, 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 by an implicit method including viscous effects : User's manual / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Stan J. Miley, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
TRANDESNF : a computer program for transonic airfoil design and analysis in nonuniform flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by Jen-Fu Chang, C. Edward Lan, and Langley Research Center (page images at HathiTrust)
An exploratory investigation of the STOL landing maneuver / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Advanced missile technology : a review of technology improvement areas for cruise missiles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Some aspects of essentially nonoscillatory (ENO) formulations for the Euler equations / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Sukumar R. Chakravarthy, Langley Research Center, and Rockwell International. Science Center (page images at HathiTrust)
The Influence of sweep on the aerodynamic loading of an oscillating NACA 0012 airfoil / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979-), by A. O. St. Hilaire and United States National Aeronautics and Space Administration (page images at HathiTrust)
Inverse design technique for cascades [microform] / ([Washington, D.C.] : 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)
Computer program to calculate three-dimensional boundary layer over wings with wall mass transfer / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Observed torque-producing forces acting on satellites / (Washington, D.C. : 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)
Measured response to wind-induced dynamic loads of a full-scale scout vehicle mounted vertically on a launching tower / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [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,. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Robert L. Jr James and United States National Aeronautics and Space Administration (page images at HathiTrust)
Survey of energy-absorption devices for soft landing of space vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Jack B. Esgar 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analysis of melting boundary layers on decelerating bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Simon Ostrach, Jesse Hamman, Arthur W. Goldstein, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Some divergence characteristics of low-aspect-ratio wings at transonic and supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Donald S. Woolston, Herbert J. Cunningham, Frederick W. Gibson, 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Harry L. Runyan, Nan H. Jones, and Langley Research Center (page images at HathiTrust)
Flutter studies to determine nacelle aerodynamic effects on a fan-jet transport model for two mount systems and two wind tunnels [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Moses G. Farmer, Langley Research Center, and United States National Aeronautics and Space Administration (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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Charles P. Llewellyn and Walter D. Wolhart (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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Robert J. Huston and Matthew M. Winston (page images at HathiTrust)
Transition Reynolds numbers of separated flows at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Howard K. Larson, Stephen J. Keating, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analytical investigation of the motion of a clamshell-type heat shield on deployment from a parent vehicle in the atmosphere / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Ross L. Goble and Langley Research Center (page images at HathiTrust)
Investigation of the flow over simple bodies at Mach numbers of the order of 20 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Arthur Henderson and Langley Research Center (page images at HathiTrust)
Deployment and performance characteristics of 5-foot-diameter (1.5 m) attached inflatable decelerators from Mach number 2.2 to 4.4 / (Washington, DC : National Aeronautics and Space Administration, 1970), by Herman L. Bohon, Robert Miserentino, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Effect of ground proximity on the longitudinal, lateral, and control aerodynamic characteristics of a tilt-wing four-propeller V/STOL model / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Victor L. Peterson, Loren G. Bright, and Ames Research Center (page images at HathiTrust)
Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Robert P. Smith, William C. Moseley, and United States. National Aeronautics and Space Administration. Space Task Group (page images at HathiTrust)
A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Kenneth C. Weston, Joanna E. Swanson, and United States. National Aeronautics and Space Administration. Space Task Group (page images at HathiTrust)
Empirical three-sigma wind component profiles 45-degree missile flight azimuth Atlantic Missle Range PAtrick AFB (Cape Canaveral), Florida / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by William W. Vaughan (page images at HathiTrust)
Automatic fixed camera orientation procedures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Wendell H. Stillwell and Terry J. Larson (page images at HathiTrust)
Full-scale wind-tunnel tests of a medium-weight utility helicopter at forward speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by John L. McCloud, Ralph L. Maki, James C. Biggers, and United States National Aeronautics and Space Administration (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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by Robert S. Dunning and United States National Aeronautics and Space Administration (page images at HathiTrust)
Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1967]), by James F. Campbell and United States National Aeronautics and Space Administration (page images at HathiTrust)
A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Thomas R. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation of a deflected-slipstream cruise-fan V/STOL aircraft wing / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
Large-scale wind-tunnel investigation of a model with an external jet-augmented flap / (Washington, D.C. : 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)
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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by Cuyler W. Brooks, Charles D. Trescot, 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by William C. Sleeman 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° to 90° / (Washington, [D.C.] : 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° / (Washington, [D.C.] : 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)
Research on blunt-faced entry configurations at angles of attack Between 60° and 90° / (Washington D.C. : National Aeronautics and Space Administration, 1960), by William H. Phillips and Langley Research Center (page images at HathiTrust)
Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° / (Washington D.C. : National Aeronautics and Space Administration, 1960), by Ross B. Robinson, Paul W. Howard, and Langley 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 / (Washington, [D.C.] : 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)
Performance of a composite solid propellant at simulated high altitudes / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Carl C. Ciepluch and Langley Research Center (page images at HathiTrust)
Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex / (Washington, D.C. : National Aeronautics and Space Administration : Scientific and Technical Information Branch, 1965), by Edward C. Polhamus, Alexander D. Hammond, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Analysis of a coupled roll-spiral-mode, pilot-induced oscillation experienced with the M2-F2 lifting body / (Washington, D.C. : 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 / (Washington, [D.C.] : 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 investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0 / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Bruce G. Chiccine, Arthur M. Shinn, Alfred S. Valerino, and Langley Research Center (page images at HathiTrust)
Static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations at Mach numbers from 1.60 to 2.86. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1971]), by Samuel M. Dollyhigh, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Natural laminar flow experiments on modern airplane surfaces / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds / (Washington, D.C. : 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)
Grid generation and flow solution method for Euler equations on unstructured grids / (Washington, D.C. : 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)
Development and validation of a combined rotor-fuselage induced flow-field computational method / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Carl E. Freeman, Army Research and Technology Laboratories (U.S.). Structures Laboratory, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Parametric study of a canard-configured trasport using conceptual design optimization / (Washington, D.C. : 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)
Semianalytic modeling of aerodynamic shapes / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Raymond L. Barger, Mary S. Adams, and Langley Research Center (page images at HathiTrust)
Downwash in the plane of symmetry of an elliptically loaded wing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985), by James D. Phillips 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], [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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by National Technical Information Service], 1984), by C. Warren Campbell 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Experimental investigation of tangential blowing applied to a subsonic V/STOL inlet / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Richard R. Burley 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 / (Washington, D.C. : 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)
Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps / (Washington, D.C. : 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)
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 ̊/ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978 i.e. 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)
Aerodynamic performance of flared fan nozzles used as inlets / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Donald A. Dietrich, Gary G. Kelm, Theo G. Keith, and Lewis Research Center (page images at HathiTrust)
NASA Aerodynamics Program, annual report 1989 / (Washington, D.C. : NASA, Scientific and Technical Information Division, 1990), by Bruce J. Holmes, United States. Office of Aeronautics and Space Technology, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Three-dimensional cavity flow fields at subsonic and transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by E. B. Plentovich and Langley Research Center (page images at HathiTrust)
Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983-), by Clyde Hayes 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by David E. Reubush and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Tests of a "D" vented thrust deflecting nozzle behind a simulated turbofan engine / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Laboratory tests of subjective reactions to sonic boom / ([Washington] : 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)
Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Larry Wayne Mohn, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
Steady subsonic flow around finite-thickness wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Ching-Chiang Kuo, L. Morino, Langley Research Center, and Boston University. Dept. of Aerospace Engineering (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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by G. F. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind tunnel interference factors for high-lift wings in closed wind tunnels / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by John DeYoung, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Engine isolation for structural-borne interior noise reduction in a general aviation aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, [Springfield, Va. : National Technical Information Service], 1981), by James F. Unruh, Dennis C. Scheidt, and Langley Research Center (page images at HathiTrust)
Subsonic panel method for the efficient analysis of multiple geometry perturbations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), by D. R. Bristow, J. Dennis Hawk, Langley Research Center, and McDonnell Aircraft Company (page images at HathiTrust)
Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Numerical analysis and FORTRAN program for the computation of the turbulent wakes of turbomachinery rotor blades, isolated airfoils and cascade of airfoils / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Integrated application of active controls (IACC) technology to an advanced subsonic transport : project plan / (Washington, D.C. : National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊/ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Techincal Information Service, 1980-1985), by John D. Stanitz and Lewis Research Center (page images at HathiTrust)
Calculation of water drop trajectories to and about arbitrary three-dimensional bodies in potential airflow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.] : For sale by the National Technical Information Service, 1980), by Hillyer G. Norment, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Aeroelastic addition to NASTRAN / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 ̊/ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Calculation of two-dimensional inlet flow fields in a supersonic free strem by an implicit marching code with nonorthogonal mesh generation : user's manual / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
A supersonic, three-dimensional code for flow over blunt bodies : user's manual / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by D. S. Chaussee, Oden J. McMillan, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
A supersonic three-dimensional code for flow over blunt bodies : program documentation and test cases / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by National Technical Information Service], 1980), by D. S. Chaussee, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
USSAERO computer program development, versions B and C / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by National Technical Information Service], 1980), by F. A. Woodward, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
An improved Woodward's panel method for calculating leading-edge and side-edge suction forces at subsonic and supersonic speed / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
A three dimensional vortex wake model for missiles at high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Calculation of aerodynamic characteristics of airplane configurations at high angles of attack / (Washington, D.C. : 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)
An approximate analytical method for studying entry into planetary atmospheres / (Washington, DC : 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)
Aerodynamic analysis of tektites and their parent bodies / (Washington, D.C. : National Aeronautics and Space Administration, 1962), by E. W. Adams and R. M. Huffaker (page images at HathiTrust)
A Theoretical study of stagnation-point ablation / (Washington, DC : U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Optimum airplane flight paths / (Washington, D.C. : National Aeronautics and Space Administration, [1959]), by Placido Cicala (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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by Dennis E. Fuller, Victor E. Langhans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Lubricating oils for aviation gas turbines / (Washington : 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)
Evaluation of an indirect viewing system for lifting-body terminal-area navigation and landing tasks / (Washington, D.C. : 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)
Flight investigation of V/STOL height-control requirements for hovering and low-speed flight under visual conditions / (Washington, D.C. : National Aeronautics and Space Administration, [1967]), by James R. Kelly, Perry L. Deal, John F. Garren, and Langley Research Center (page images at HathiTrust)
Full-scale investigation of the aerodynamic characteristics of a model employing a sailwing concept / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Marvin P. Fink, 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Walton L. Howes and Lewis Research Center (page images at HathiTrust)
Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Office, 1977), by James M. Luckring and United States National Aeronautics and Space Administration (page images at HathiTrust)
A modified method of integral relations approach to the blunt-body equilibrium air flow field, including comparisons with inverse solutions / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151], 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 / (Washington, D.C. : 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)
Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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)
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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Arvid L. Keith, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Fixed-base visual simulation of obstacle avoidance during terminal descent of advanced Apollo spacecaft with an all-flexible parawing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by G. Kimball Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effects of pressure distributions on bluff tension-shell shapes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and technical Information, Springfield, Va. 22151], 1970), by James Wayne Sawyer, 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 / (Washington, D.C. : 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)
Effects of jet-exhaust location on the longitudinal aerodynamic characteristics of a jet V/STOL model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1969), by Arthur W. Carter, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Wind-tunnel investigation of V/STOL transport model with six wing-mounted lift fans / (Washington, D.C. : 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)
Noise produced by a small-scale, externally blown flap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by William A. Olsen, Robert G. Dorsch, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Aerodynamic parameters of the Navion airplane extracted from flight data / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by William T. Suit, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Exploratory flight investigation of aircraft response to the wing vortex wake generated by jet transport aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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)
Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [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 / (Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970), by Richard J. Margason, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston. (Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970), by Matthew M. Winston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
A theoretical and experimental study of unsteady flow processes in a Ludwieg tube wind tunnel / (Washington, D.C. : 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)
Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by E. B. Klunker, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
A Fortran program to calculate the flow field and performance of an axially symmetric deLaval nozzle / (Washington, D.C. : 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)
Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by Charles C. Smith, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
Analytical and experimental investigation of the coaxial plasma gun for use as a particle accelerator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Edward L. Shriver, George C. Marshall Space Flight 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 / (Washington, DC : 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)
Resistance of air and the question of flying. Experimental lecture read by Arnold Samuelson ... (Hamburg, Boysen & Maasch; New York, Spon & Chamberlain;, [etc., etc.] 1905), by Arnold Samuelson (page images at HathiTrust; US access only)
Elementary laboratory aerodynamics, (New York, The Ronald press company, [c1929]), by Arthur L. Jordan (page images at HathiTrust)
Aufgaben aus der technischen Mechanik. (Berlin, J. Springer, 1907-11), by Ferdinand Wittenbauer (page images at HathiTrust; US access only)
Some effects of flight path and atmospheric variations on the boom propagated from a supersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration, 1964), by Raymond L. Barger, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
Reynolds number effects on the induced pressures of cylindrical bodies with different nose shapes and nose drag coefficients in helium at a Mach number of 24 / (Washington, D.C. : 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)
Heat-transfer measurements on a flat plate and attached fins at Mach numbers of 3.51 and 4.44 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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)
Large-scale wind-tunnel investigation of an M1-L lifting body with an inflatable and a rigid afterbody / (Washington, D.C. : 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)
Unsteady aerodynamic forces on subsonic aircraft exposed to blast gusts of arbitrary orientation (Wright-Patterson Air Force Base, O., 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)
Aeroelasticity symposium ... April 16-17, 1957. (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Germany) Aeroelastisches Kolloquim (1957 : Göttingen (page images at HathiTrust)
Characteristics of dilute gas-solids suspensions in drag reducing flow / (Washington, D.C. : National Aeronautics and Space Administration, 1973), by Ronald Steven Kane (page images at HathiTrust; US access only)
Some aspects of the behavior of perforated transonic wind tunnel walls. (Providence, 1954), by P. F. Maeder (page images at HathiTrust; US access only)
Empirically determined wind and scale effects on hot gas recirculation characteristics of jet V/Stol aircraft, (Washington, D.C., 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)
Flow and acoustic characteristics of subsonic and supersonic jets from convergent nozzle / (Washington, D.C. : 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)
A review of the planform effects on the low-speed aerodynamic characteristics of triangular and modified triangular wings / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by A. S. Hersh, J. C. Slattery, and J. F. Friichtenicht (page images at HathiTrust; US access only)
A method of calculating wind tunnel interference factors for tunnels of arbitrary cross-section / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Robert G. Joppa (page images at HathiTrust; US access only)
Applied aerodynamics / (New York ; London [etc.] : Longmans, Green and co., 1920), by Leonard Bairstow (page images at HathiTrust; US access only)
La résistance de l'air et l'aviation; expériences effectuées au Laboratoire du Champ-de-Mars, (Paris, H. Dunod et E. Pinat, 1910), by Gustave Eiffel (page images at HathiTrust; US access only)
Die Luft in Lichte der Lüftungstechnik. (Halle a. S.: C. Marhold, 1913), by Johannes Kelling (page images at HathiTrust; US access only)
Aerodynamics for naval aviators / ([Washington, D.C.] : 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)
Pursuit of power : NASA's Propulsion Systems Laboratory, No. 1 & 2 /, by Robert S. Arrighi and United States. NASA History Division (page images at HathiTrust)
The mechanics of the aeroplane; a study of the principles of flight, (London, New York [etc.] Longmans, Green and Co., 1915), by Émile August Duchêne and John Henry Ledeboer, trans. by Thomas O'Brien Hubbard (page images at HathiTrust; US access only)
Viscous flow in a short cylindrical vortex chamber with a finite swirl ratio / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Robert W. Hornbeck, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
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)
Die Gesetze des Gleichgewichts und der Bewegung flüssiger Körper / (Leipzig : Bey Siegfried Lebrecht Crusius, 1806), by Leonhard Euler and H. W. Brandes (page images at HathiTrust)
Preliminary report on a study of separated flows in supersonic and subsonic streams / (Washington : 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)
Effect of flow rate on the dynamic contact angle for wetting liquids / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Thom A. Coney, William J. Masica, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Stability of constant-gain systems with vector feedback / (Washington, D.C. : 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)
Ergebnisse der Aerodynamischen Versuchsanstalt zu Göttingen. (München und Berlin, R. Oldenbourg, 1921-1932), by Aerodynamische Versuchsanstalt Göttingen, Albert Betz, Carl Wieselsberger, and Ludwig Prandtl (page images at HathiTrust; US access only)
Effects of boundary layer buildup in shock tubes upon chemical rate measurements / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Marvin Warshay, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Analysis of boiling on a fin / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Y. Y. Hsu, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Forces and moments due to air jets exhausting parallel to large flat plates in a near vacuum / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Joseph J. Janos, Sherwood Hoffman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Large-scale tests of an airplane model with a double-Delta wing, including longitudinal and lateral characteristics and ground effects / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Victor R. Corsiglia, Joseph P. Morelli, David G. Koenig, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Response of an infinite elastic plate to axisymmetric initial velocity distributions with application to hypervelocity impact / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Robert J. Hayduk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Heat-transfer and pressure distributions on spherically blunted 25 ̊half-angle cone at Mach 8 and angles of attack up to 90 ̊/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Dennis M. Bushnell, Jarrett K. Huffman, Robert A. Jones, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Flight investigation of the effects of Apollo heat-shield singularities on ablator performance / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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)
Les lois expérimentales de l'aviation, (Paris, Librairie aéronautique, 1911), by Alexandre Sée (page images at HathiTrust; US access only)
Experimental aerodynamics, (New York, Chicago, Pitman publishing corporation, [c1940]), by Henry Christensen Pavian and Phillip Lincoln Michel (page images at HathiTrust)
Basic fluid mechanics. (New York : McGraw-Hill, 1963), by J. Lister Robinson (page images at HathiTrust)
Prediction of windage power loss in alternators / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by James E. Vrancik, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Sustentation, propulsion, évolution de l'aéroplane. (Paris, Librairie aéronautique, 1910), by Henri Dujardin (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. (Washington, U.S. Govt. Print. Off., 1938), by United States. Army-Navy-Commerce Committee on Aircraft Requirements (page images at HathiTrust)
Methods of linearization in compressible flow. (Dayton, Ohio, 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)
Isoperimetrische aufgaben aus der theorie des fluges ... (Göttingen, Dieterichsche universitäts-buckdruckerei, 1919), by Max M. Munk (page images at HathiTrust; US access only)
L'aviation, (Paris, F. Alcan, 1911), by Paul Painlevé and Emile Borel (page images at HathiTrust; US access only)
L'aviation, (Paris, F. Alcan, 1913), by Paul Painlevé, Charles Maurain, and Emile Borel (page images at HathiTrust; US access only)
Fliegerkraftlehre, (Leipzig, 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, (Paris, H. Dunod et E. Pinat, 1910), by Gustave Eiffel (page images at HathiTrust; US access only)
Résumé des principaux travaux exécutés pendant la guerre au Laboratoire aérodynamique Eiffel, 1915-1918, (Paris, Librairie aéronautique, E. Chiron, éditeur, [1919]), by Gustave Eiffel (page images at HathiTrust; US access only)
Aérodonétique, (Paris, Gauthier-Villars et cie, 1916), by F. W. Lanchester, trans. by C Benoit (page images at HathiTrust; US access only)
Aeronautics in theory and experiment, (London, E. Arnold, 1920), by W. L. Cowley and H. Levy (page images at HathiTrust; US access only)
Fundamentals of fluid dynamics for aircraft designers / (New York : The Ronald press company, [c1929]), by Max M. Munk (page images at HathiTrust)
The theory and performance of axial-flow fans, (New York, London, McGraw-Hill Book Co., 1937), by Curt Keller, John Robert Weske, and Lionel S. Marks (page images at HathiTrust; US access only)
Bases théoriques de l'aéronautique. (Paris, Gauthier-Villars et cie, 1916), by Nikolaĭ Egorovich Zhukovskiĭ and S. Drzewiecki (page images at HathiTrust; US access only)
Mécanique de l'aviation; application des méthodes de la mécanique rationnnelle à l'étude du vol et de la construction des avions. (Paris, Gauthier-Villars et cie, [1925]), by Antoine Charles Alayrac (page images at HathiTrust; US access only)
Aerodynamics of the aeroplane, (New York, The Ronald press company, [1944]), by W. L. Cowley (page images at HathiTrust)
Recherches expérimentales sur la résistance de l'air exécutées à la tour Eiffel, (Paris, Librairie aéronautique, [1909]), by Gustave Eiffel (page images at HathiTrust; US access only)
Dynamics of airplanes and airplane structures / (New York : J. Wiley, 1931), by John E. Younger and Baldwin Munger Woods (page images at HathiTrust)
High-speed aerodynamics. (New York, Prentice-Hall, 1948), by Harold Ward Sibert (page images at HathiTrust)
Original solutions of several problems in aerodynamics. (New Haven, Tuttle, Morehouse & Taylor, printers, 1882), by Eli W. Blake (page images at HathiTrust)
Die mechanischen grundgesetze der flugtechnik unter der vereinfachenden annahme konstanten spezifischen volumens der atmosphärischen luft. (Wien, Selbstverlag des verfassers, kommissionsverlag von Lehmann & Wentzel, 1904), by Arthur Budau (page images at HathiTrust; US access only)
Die hydrodynamischen grundlagen des fluges, (Braunschweig, F. Vieweg & sohn, 1917), by R. Grammel and Fritz Emde (page images at HathiTrust; US access only)
Technical aerodynamics. (Ann Arbor, Distributed by Ulrich's Book Store, [1955]), by Karl Dawson Wood (page images at HathiTrust)
Über die wirkungsweise zylindrischer sonden zur untersuchung aërodynamischer felder ... (Basel, Buchdruckerei E. Birkhäuser & cie., 1920), by Fritz Ebi (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)
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)
Gas dynamics tables for air. (New York, Dover Publications, [1948, c1947]), by H. W. Emmons (page images at HathiTrust)
The resistance of the air and aviation experiments conducted at the Champ-de-Mars laboratory, (London, 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)
The aerodynamics of powered flight. (New York : Wiley, [1960]), by Robert Leon Carroll (page images at HathiTrust)
Modern flight dynamics. (Englewood Cliffs, N.J., Prentice-Hall, 1961), by W. Richard Kolk (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-), by James R. Hansen (page images at HathiTrust)
A detailed development of the tricyclic theory / ([Albuquerque, N. M. : Sandia Laboratories], 1968), by Harold R. Vaughn and Sandia Corporation (page images at HathiTrust; US access only)
L'aviation; ses debuts--son développement; (Paris, Nancy, Berger-Levrault & cie, 1908), by Ferdinand Ferber (page images at HathiTrust; US access only)
Basic wing and airfoil theory. (New York, McGraw-Hill, 1951), by Alan Pope (page images at HathiTrust)
Der schwebflug und die fallbewegung ebener tafeln in der luft. (Hamburg, L. Friederichsen & co., 1897), by Friedrich Ahlborn (page images at HathiTrust; US access only)
The analytical development of curves and streamline shapes. (Amityville, N.Y., Deemar Co., c1948), by Harry Hermann Haase (page images at HathiTrust)
Führer durch die strömungslehre, ([Ann Arbor, Mich. J.W. Edwards, 1947]), by Ludwig Prandtl (page images at HathiTrust)
Principles of aerodynamics. (New York, McGraw-Hill, [1949]), by James H. Dwinnell (page images at HathiTrust)
Theorie und Praxis der Flugtechnik / (Berlin : R.C. Schmidt, 1911), by Paul Painlevé, A. Schöning, and Emile Borel (page images at HathiTrust; US access only)
Fluid dynamics and applications, ([New York] 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 ... (Göttingen, Vandenhoeck und Ruprecht, 1831), by Johann Karl Eduard Schmidt (page images at HathiTrust)
Bibliography of vibration and flutter of aircraft wings and control surfaces, ([New York?], 1937), by United States. Work Projects Administration and Alexander Klemin (page images at HathiTrust)
L'aviation, (Paris, F. Alcan, 1911), by Paul Painlevé and Emile Borel (page images at HathiTrust; US access only)
Aircraft design data ... (Washington, Govt. print. off., 1919), by United States. Navy Department. Bureau of Construction and Repair (page images at HathiTrust)
Aerodonetics : constituting the second volume of a complete work on aerial flight / (London : A. Constable, 1908), by F. W. Lanchester (page images at HathiTrust)
Smoke streams : visualized air flow / (New York : Coward-McCann, 1943), by Charles Townsend Ludington (page images at HathiTrust)
Lois mathématiques de la résistance des fluides. Théorie de l'hélice, (Paris, O. Doin, 1921), by Henri Louis Émile Willotte (page images at HathiTrust; US access only)
Die verwendung des Wellenkampschen schleppsystems für aerodynamische untersuchungen ... (Kiel, Druck von C. Donath, 1914), by Albert Sommer (page images at HathiTrust; US access only)
Causeries techniques sans formules sur l'aéroplane. (Paris, Librairie aéronautique, 1913), by Émile Auguste Duchêne (page images at HathiTrust; US access only)
Flight with out formulæ. (London ; New York [etc.] : Longmans, Green and co., 1916), by Emile Duchêne, trans. by John H. Ledeboer (page images at HathiTrust; US access only)
Théorie des hélices propulsives marines et aériennes et des avions en vol rectiligne, (Paris, Gauthier-Villars et cie, 1920), by Auguste Rateau (page images at HathiTrust; US access only)
Aerodynamics / (New York ; London : McGraw-Hill, 1946), by A. Wiley Sherwood (page images at HathiTrust; US access only)
Mathematics of flight / (New York ; London : McGraw-Hill book company, inc., [c1943]), by James Naidich (page images at HathiTrust; US access only)
Simple aerodynamics and the airplane, (New York, The Ronald Press Company, [c1940]), by Clifton Carroll Carter (page images at HathiTrust)
Introduction to aerodynamics of a compressible fluid, (New York Wiley, [1948, c1947]), by H. W. Liepmann and Allen E. jt Puckett (page images at HathiTrust)
Théorie des surgaces portantes; la théorie de Prandtl, ([Paris, Gauthier-Villars et cie, 1923]), by Maurice Roy (page images at HathiTrust; US access only)
Ergebnusse der Aerodynamischen Versuchsanstalt zu Göttingen. (München [etc.], R. Oldenbourg.), by Aerodynamische Versuchsanstalt Göttingen (page images at HathiTrust; US access only)
La résistance de l'air et le vol des oiseaux, (Paris, Gauthier-Villars, 1911), by Maurice Gandillot (page images at HathiTrust; US access only)
Grundlagen der flugtechnik; (Leipzig-Berlin, B. G. Teubner, 1920), by H. G. Bader (page images at HathiTrust; US access only)
Aerodynamics for model airplanes; how and why a model airplane flies, (New York, A. S. Barnes, [1952]), by Donald K. Foote (page images at HathiTrust)
Vorträge aus dem gebiete der hydro- und aerodynamik (Innsbruck 1922) (Berlin, J. Springer, 1924), by Theodore Von Kármán, ed. by Tullio Levi-Civita (page images at HathiTrust; US access only)
Principles of aerodynamics. (New York, Pitman Pub. Corp., [1953]), by Daniel O. Dommasch (page images at HathiTrust)
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Aircraft wake vortices : an annotated bibliography (1923-1990) / (Washington D.C. : Federal Aviation Administration, Research and Development Service ; Springfield, Va. : Available through the National Technical Information Service, [1991]), by J. N. Hallock, John A. Volpe National Transportation Systems Center (U.S.), and United States. Federal Aviation Administration. Research and Development Service (page images at HathiTrust)
L'aéroplane étudié et calculé par les mathématiques élémentaires. (Paris, R. Chapelot & cie, 1910), by Émile Auguste Duchêne (page images at HathiTrust; US access only)
The measurement of fluid velocity and pressure, (London, E. Arnold & co., 1924), by John Robert Pannell, ed. by Robert Alexander Frazer (page images at HathiTrust; US access only)
Aerodynamics, : constituting the first volume of a complete work on aerial flight, / (London : A. Constable, 1907), by F. W. Lanchester (page images at HathiTrust; US access only)
Performance of trailing aerodynamic decelerators at high dynamic pressures : Phases V and VI /, by B. A. Engstrom, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (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 /, by Lloyd E. Wilkie, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (page images at HathiTrust)
Airplane aerodynamics, (New York, Pitman Pub. Corp., [1951]), by Daniel O. Dommasch (page images at HathiTrust)
Bibliography on skin friction and boundary flow, (Washington, D.C., 1932 [i. e., 1933]), by Library of Congress. Division of Aeronautics, Cecil Alured Ross, and Albert Francis Zahm (page images at HathiTrust)
Passive aerodynamic attitude stabilization of near earth satellites /, by sponsor United States. Air Force. Air Force Systems Command. Aeronautical Systems Division, O. C. Juelich, Paul H. Davidson, D. M. Schrello, and issuing body Wright Air Development Division (page images at HathiTrust)
Computation curves for compressible fluid problems, (New York, J. Wiley, [1949]), by Charles Lee Dailey and Frances Caldwell Wood (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 /, by Yudell L. Luke, Frank Wagner, Geraldine V. Coombs, United States. Air Force. Air Research and Development Command. sponsor, Midwest Research Institute, and Wright Air Development Center (page images at HathiTrust)
Drag due to lift of a not-so-slender configuration /, by Hsien K. Cheng, United States. Air Force. Air Research and Development Command. sponsor, Inc Cornell Aeronautical Laboratory, and Wright Air Development Center (page images at HathiTrust)
The elements of aerofoil and airscrew theory, (Cambridge [Eng.] The University Press, 1926), by H. Glauert (page images at HathiTrust)
Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Bernard N. Daley, Richard S. Dick, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Aeroplane designing for amateurs / (Chicago : Reilly & Britton, 1912), by Victor Lougheed (page images at HathiTrust)
Air forces on circular cylinders, axes normal to the wind, with special reference to dynamical similarity / ([Washington, D.C. : U.S. Dept. of Commerce, Bureau of Standards : U.S. Govt. Print. Off., 1920]), by Hugh L. Dryden and United States. National Bureau of Standards. Scientific Papers (page images at HathiTrust)
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Location of detached shock wave in front of a body moving at supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Edmund V. Laitone, Otway O'M. Pardee, and United States. National Advisory Committee for Aeronautics. NACA research memorandum (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 / (Washington, DC : National Advisory Committee for Aeronautics, 1947), by Emmet A. Mossman, Donald E. Gault, and United States. National Advisory Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Low-speed characteristics in pitch of a 34⁰ sweptforward wing with circular-arc airfoil sections / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by D. William Conner, Patrick A. Cancro, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Melvin M. Carmel, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Flow of heated gases /, by A. S. Thompson, North American Aviation, and U.S. Atomic Energy Commission (page images at HathiTrust)
Two-component force balance for measuring skin friction and side force /, by Eugene V. Horanoff, Richard T. Driftmyer, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
Technische berichte. ([Berlin] Gedruckt in der Reichsdruckerei.) (page images at HathiTrust; US access only)
Introduction to aeronautical dynamics. (New York : Wiley, 1953), by Manfred Rauscher (page images at HathiTrust)
L'aviation; conferences faites en 1909 à la Société d'encouragement pour l'industrie nationale. (Paris, H, Dunod et E. Pinat, 1909), by Paul Renard (page images at HathiTrust; US access only)
Aerodynamics for pilots, (Washington, U.S. Govt. print. off., 1940), by Bradley Jones (page images at HathiTrust; US access only)
General theory of conical flows and its application to supersonic aerodynamics / (Washington, D.C. : NACA, 1955), by Paul Germain 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 / (Washington, D.C. : NACA, 1953), by V. I. Yatseyev and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight measurements of airplane structural temperatures at supersonic speeds / (Washington, D.C. : NACA, 1957), by Richard D. Banner, United States. National Advisory Committee for Aeronautics, and Flight Research Center (U.S.) (page images at HathiTrust)
Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel / (Washington, D.C. : NACA, 1958), by Joseph W. Jewel, Robert D. Harrington, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Sound measurements for five shrouded propellers at static conditions / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Harvey H. Hubbard, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (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 / (Washington, D.C. : 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. NACA research memorandum (page images at HathiTrust)
Experimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Leo T. Chauvin, Joseph P. Maloney, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
The rolling moment due to sideslip of swept wings at subsonic and transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Edward C. Polhamus, William C. Sleeman, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Douglas R. Lord, Robert Moring, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Richard E. Kuhn, Andrew L. Byrnes, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by James W. Wiggins, Richard E. Kuhn, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Use of Freon-12 as a fluid for aerodynamic testing / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1946), by Paul W. Huber 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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©� / (Washington, D.C. : 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 / (Washington, D.C. : 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)
The design of wind tunnels and wind tunnel propellers / (Washington, D.C. : G.P.O., 1919), by Edward P. Warner, C. M. Herbert, F. H. Norton, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Effect of roughness on properties of airfoils / (Washington, D.C. : 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 / (Cincinnati, Ohio : 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)
A slide rule type of device to measure logarithmic decay times as presented by oscillograph records / (Albuquerque, N.M. : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1960]), by Rodman Leach, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
The Effect of simulated icing on propeller performance / (Washington D.C. : 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)
The determination of aerodynamic stability coefficients from rocket flight test data / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1961]), by A. C. Bustamante and Sandia Corporation (page images at HathiTrust)
Aerodynamic derivatives for both steady and non-steady motion of slender bodies /, 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 /, 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 gases in constant-area passages with friction and arbitrary heat addition /, by M. P. Heisler, E. Martin, H. Sletten, U.S. Atomic Energy Commission, and North American Aviation (page images at HathiTrust)
How to analyze 2-D Schlieren photographs to obtain the density gradient structure of 3-D flow fields /, by Allen E. Winkelmann, Robert H. Feldhuhn, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Handbook of blunt-body aerodynamics: volume 1 - static stability. /, 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. /, by Arnold Polak and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Flight without formulae; simple discussions on the mechanics of the aeroplane, (London, New York [etc.] Longmans, Green and co., 1916), by Émile Auguste Duchêne and John Henry Ledeboer (page images at HathiTrust; US access only)
The theories of turbulence / (Washington, D.C. : NACA, 1955), by L. Agostini, J. Bass, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
CAST-10-2/DOA 2 Airfoil Studies Workshop results : proceedings of a workshop / (Washington, D.C. : NASA, Office of Management, Scientific and Technical Information Division, 1989), by CAST-10-2/DOA 2 Airfoil Studies Workshop (1988 : NASA Langley Research Center), Acquilla S. Hill, and Edward J. Ray (page images at HathiTrust)
NACA research memorandum. (Washington : National Advisory Committee for Aeronautics,), by United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Standard aeronautical symbols /, by issuing body United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Tables of interference factors for use in wind-tunnel and ground-effect calculations for VTOL-STOL aircraft. (Washington, National Aeronautics and Space Administration, 1962), by Harry H. Heyson (page images at HathiTrust; US access only)
An investigation of the dynamic stability and control characteristics for a transport cruising at a Mach number of 3 / (Washington, D.C. : 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)
Subsonic and transonic flutter and flow investigations of the T-tail of a large multijet cargo airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Maynard C. Sanford, E. Carson Yates, Charles L. Ruhlin, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Subsonic and supersonic flutter analysis of a highly tapered swept-wing planform, including effects of density variation and finite wing thickness, and comparison with experiments / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by E. Carson Yates, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
A preliminary determination of normal accelerations on racing airplanes / (Washington, D.C. : 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)
Wing roll control devices for transonic high lift conditions., by Jack D. McAllister, Perry D. Whitten, David B. Benepe, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor General Dynamics Corporation. Convair Division (page images at HathiTrust)
Wing roll control devices for transonic high lift conditions., by Jack D. McAllister, Perry D. Whitten, David B. Benepe, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor General Dynamics Corporation. Convair Division (page images at HathiTrust)
Development of an empirically based computer program to predict the aerodynamic characteristics of aircraft., by M. L. Goldhammer, C. C. Shen, M. L. Lopez, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Douglas Aircraft Company (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
Evaluations of methods to predict flutter of wings with external stores /, by Sidney Siegel, Lowell V. Andrew, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor North American Rockwell Corporation (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
Operating points, particle dynamics, and coordinate systems for aerospace vehicle stability and control /, by Duane T. McRuer, Irving Ashkenas, issuing body United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor 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 /, by Walter J. Mykytow, Michael H. Shirk, Lawrence J. Huttsell, Thomas E. Noll, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (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 /, by James F. Quinn, Richard H. Gallagher, Donald Turrentine, sponsor Bell Aircraft Corporation, sponsor United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command. issuing body (page images at HathiTrust)
Calculation of laminar separation with free interaction by the method of integral relations., by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, sponsor Wright-Patterson Air Force Base (Ohio), sponsor Itek Corporation, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Response of aircraft encountering aircraft wake turbulence /, by Robert C. Nelson and sponsor 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 / ([Providence, R.I.] : Graduate Division of Applied Mathematics, Brown University, 1948), by Alexander A. Nikolsky and G. I. Taganoff (page images at HathiTrust)
Contributions to the theory of the spreading of a free jet issuing from a nozzle / (Washington, D.C. : NACA, 1951), by W. Szablewski and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
The flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 / (Washington, D.C. : NACA, 1954), by W. F. Lindsey, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications / (Washington, D.C. : NACA, 1952), by Patrick L. Donoughe, Roy A. McKinnon, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Abriss der Lehre von der Flüssigkeits- und Gasbewegung / (Jena : G. Fischer, 1913), by Ludwig Prandtl (page images at HathiTrust; US access only)
Mechanical engineering report. (Ottawa.), by National Research Council Canada (page images at HathiTrust; US access only)
Étude sur l'aviation, (Paris Liége, C. Béranger, 1909), by Maurice de Cantelou (page images at HathiTrust; US access only)
Flugtechnik; (München und Berlin, R. Oldenbourg, 1919), by Arthur Pröll (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, (Berlin, J. Springer, 1925), by H. Croseck (page images at HathiTrust; US access only)
Applied wing theory / (New York ; London : McGraw-Hill book company, inc., 1932), by Elliott Gray Reid (page images at HathiTrust; US access only)
Théorie du vol des avions, (Paris, É. Chiron, 1920), by Rodolphe Soreau (page images at HathiTrust; US access only)
Sailing aerodynamics. (New York, Philosophical Library, 1954), by John Morwood (page images at HathiTrust)
Aerodynamik, (Berlin, R. C. Schmidt & co., 1922), by Richard Fuchs and Ludwig Hopf (page images at HathiTrust; US access only)
Selected topics in fluid mechanics, Summer session 1946 [New York University?] ([New York?], 1946), by K. O. Friedrichs (page images at HathiTrust)
Simple aerodynamics and the airplane / (New York : The Ronald press company, c1929), by Clifton Carroll Carter and Charles Norton Monteith (page images at HathiTrust)
Die gesetze des gleichgewichts und der bewegung flüssiger körper. (Leipzig. S.L. Crusius, 1806), by Leonhard Euler, trans. by H. W. Brandes (page images at HathiTrust)
An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane / (Washington, D.C. : National Advisory Committee for Aeronautics, [1951]), by Richard B. Skoog, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
An evaluation of two cooling-air ejectors in flight at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1954]), by L. Stewart Rolls, C. Dewey Havill, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
The effects of compressibility on the upwash at the propeller planes of a four-engine tractor airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by Armando E. Lopez, Jerald K. Dickson, United States. National Advisory Committee for Aeronautics. NACA research memorandum, 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1954]), by George C. Kenyon, Robert M. Reynolds, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
Festigkeitslehre und Materialkunde für das Flugwesen. (Berlin-Charlottenburg : 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. (Paris, Librairie aéronautique, 1910), by Louis Marie Le Dantec (page images at HathiTrust; US access only)
Aerodynamik; ein Gesamtwerk über das Fliegen, (Leipzig, Berlin, B.G. Teubner, 1909-11), by F. W. Lanchester and Carl Runge, trans. by A. Runge (page images at HathiTrust; US access only)
Spiral motions of viscous fluids / (Washington, D.C. : NACA, 1953), by Georg Hamel and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Approximate method of integration of laminar boundary layer in incompressible fluid / (Washington, D.C. : NACA, 1951), by L. G. Loĭt�si�anskiĭ and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Gas flow with straight transition line / (Washington, D.C. : NACA, 1951), by L. V. Ovsi�annikov and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Mathematical theory of compressible fluid flow (New York, Academic Press, 1958), by Richard Von Mises (page images at HathiTrust)
Viscous flow past a rotating translating blade with arbitrary velocity suction and slip (U) / (Albuquerque, New Mexico ; 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 / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1959]), by Alphonse Iacoletti and Sandia Corporation (page images at HathiTrust; US access only)
Survey of methods for the determination of the subsonic flow characteristics of heated gases / (Livermore, CA : 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 / (Albuquerque, New Mexico : Sandia Corporation, 1965), by A. D. Foster, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
Flight measurements of the flying qualities of five light airplanes / (Washington, D.C. : 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 / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [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 / (Washington, D.C. : 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)
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 /, 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)
Handbook of inviscid sphere-cone flow fields and pressure distributions /, by A. M. Morrison, Naval Surface Weapons Center. White Oak Laboratory, R. E. Ferguson, M. Ciment, and J. M. Solomon (page images at HathiTrust)
Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams / (Washington, D.C. : NACA, 1954), by Frederick S. Simmons, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
Caratteristiche aerodinamiche di ali. (Roma : Tipografia Befani, 1925-), by Italy. Direzione generale del genio aeronautico (page images at HathiTrust; US access only)
Essais d'aérodynamique. (Paris : [s.n.], 1911-), by Armand Antoine Agénor de Gramont (page images at HathiTrust; US access only)
Translated abstracts of Technische berichte, 1917- . ([London?], 1925-), by Aerodynamische Versuchsanstalt Göttingen and Great Britain. Air Ministry (page images at HathiTrust; US access only)
Problem of slip flow in aerodynamics / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Robert E. Street and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Aerodynamics of the psychrometer, (Newark, Del., University of Delaware, [c1926]), by George Porter Paine (page images at HathiTrust)
Studies on dynamics and instrumentation of the Holloman track /, by Air Force Missile Development Center (U.S.) and Knox Millsaps (page images at HathiTrust)
Low speed aerodynamics for ultra-quiet flight /, by R. A. Kroeger, T. C. Helvey, H.D. Gruschka, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Tennessee (System). Space Institute (page images at HathiTrust)
Allowable stresses for elevated temperature structures /, by C. G. Swanson, P. C. Huang, C. J. Van der Maas, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor Martin Marietta Corporation. Baltimore Division, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Tests to determine subsonic aerodynamic characteristics of hypersonic re-entry configurations /, by K. Mantz, R. Ross, D. B. Seager, sponsor Aeronautical Systems Center (U.S.), issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Lockheed-California Company (page images at HathiTrust)
Mach 0.6 to 3.0 flows over rectangular cavities /, by Louis G. Kaufman, Rodney L. Clark, Algirdas Maciulaitis, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Grumman Aerospace Corporation. Research and Development Center (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
Hybrid aerodynamic methods /, by Frank A. Dvorak, Donald W. Roberts, Gerald C. Paynter, T. S. Vaidyanathan, James K. Nathman, Brian Maskew, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Boeing Military Airplane Company, and Inc. Analytical Methods (page images at HathiTrust)
Aerodynamic analysis of a fighter aircraft with a higher order paneling method /, by A. R. Dusto, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Boeing Military Airplane Company (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
A Source-Doublet approach to modeling triple ejector rack store configurations and force calculations /, by Calvin L. Dyer, Charles B. Heath, issuing agency Air Force Wright Aeronautical Laboratories, and sponsor 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 /, by Frank H. Durgin, C. J. Bartlett, sponsor United States. Air Force. Systems Command. Research and Technology Division, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor Massachusetts Institute of Technology, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
The method of characteristics for three-dimensional real-gas flows : including the digital computer program details and operating procedures for frozen flows /, by Charles R. Strom, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
Determining air reactions on moving vehicles /, by Zbigniew Krzywoblocki, sponsor 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)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, Aeronautical Research Laboratory, and sponsor University of Chicago (page images at HathiTrust)
The effects of time-varying aerodynamic coefficients on aeroelastic response /, by Richard H. MacNeal, Bernard Mazelsky, Jack H. Hill, Aerospace Medical Laboratory. sponsor, sponsor United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command. issuing body (page images at HathiTrust)
Correlation of aerodynamic stability and control derivatives obtained from flight tests and wind tunnel tests on the XC-142A airplane /, by Ernest L. Black, George C. Booth, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor LTV Aerospace Corporation (page images at HathiTrust)
Aerodynamic studies : the forces acting on an air vehicle; a review of the literature /, by Zbigniew Krzywoblocki, sponsor United States. Air Force. Air Research and Development Command, Wright Air Development Center. issuing body, Wright Air Development Center, and sponsor University of Chicago (page images at HathiTrust)
Preliminary experiments on the simulation of gusts in a wind tunnel /, by Arnold M. Kuethe, R. L. Roensch, L. C. Garby, J. D. Schetzer, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Michigan. Department of Aeronautical Engineering (page images at HathiTrust)
Exact vorticity solutions of the incompressible Navier-Stokes equations /, by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
A mathematical investigation of water droplet trajectories / ([San Antonio, Tex.?] : Army Air Forces Headquarters, Air Technical Service Command ; Washington, D.C. : Distributed by Office of the Publication Board, Dept. of Commerce, 1946), by Irving Langmuir, Katherine Blodgett, and United States. Army Air Forces (page images at HathiTrust)
Considerations on the structure of mixed subsonic-supersonic flow patterns /, by Karl Gottfried Guderley and issuing agency United States. Army Air Forces. Air Matériel Command (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 / (Washington [D.C.] : 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)
Hypersonic gas dynamic charts for equilibrium air / ([Everett, Massachusetts] : Avco Research Laboratory, Avco Manufacturing Corporation, 1957), by Saul Feldman and Avco Corporation (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)
Structural weight analysis; general method: wing structures. (Santa Monica, Calif., Rand Corp., c1949), by F. R. Shanley and Rand Corporation (page images at HathiTrust; US access only)
Numerical analysis of turbulent separated subsonic diffuser flows /, by J. C. Chien, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
A survey of transition research at AEDC /, by Jack D. Whitfield, N. Sam Dougherty, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
Aerodynamic analysis for the design environment (AANDE)., by M. H. Love, D. D. Egle, sponsor Lockheed Martin. Tactical Aircraft Systems, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Holographic interferometry measurements of subsonic turbulent boundary layers /, by D. W. Sinclair, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
Pressure distributions on three rigid wings simulating parawings with varied canopy curvature and leading-edge sweep at Mach numbers from 2.29 to 4.65 / (Washington, D.C. : 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)
Feedback control for aerodynamics : preprint /, by R. Chris Camphouse, James H. Myatt, Seddik M. Djouadi, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Comparisons of free-flight and wind tunnel data on slender cones /, by B. J. Griffith, Leo G. Siler, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
The mechanical principles of the aeroplane, (London, J. & A. Churchill, 1921), by Selig Brodetsky (page images at HathiTrust; US access only)
The mechanics of the aeroplane : a study of the principles of flight. (London ; New York [etc.] : Longmans, Green and co., 1912), by Emile Duchêne, trans. by T. O'B. Hubbard and John H. Ledeboer (page images at HathiTrust; US access only)
The drag of cones, plates, and hemispheres in the wake of a forebody in subsonic flow /, by Helmut G. Heinrich, Eugene L. Haak, sponsor University of Minnesota. Department of Aerospace Engineering and Mechanics, and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
The compressible viscous layer in rarefied hypersonic flow /, by Hung-Ta Ho, Ronald F. Probstein, United States. Air Force. Aeronautical Research Laboratories. issuing body, and Brown University. Division of Engineering. sponsor (page images at HathiTrust)
Stability theory for cross hatching., by Lester Lees, Denny R. S. Ko, T. Kubota, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor California Institute of Technology (page images at HathiTrust)
Measurement and analysis of the external unsteady pressures on the airborne laser laboratory /, by Leonard J. Otten and United States. Air Force. Air Force Weapons Laboratory. issuing body (page images at HathiTrust)
Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip /, by George F. Widhopf, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)
NASA technical report. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce,), by United States National Aeronautics and Space Administration (page images at HathiTrust)
High alpha aerodynamics /, by Inc ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Influence of structural and aerodynamic modeling on flutter analysis and structural optimization /, by Alfred G. Struz, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and sponsor University of Oklahoma. School of Aerospace and Mechanical Engineering (page images at HathiTrust)
Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil /, by John C. Adams, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Applied aerodynamics, (London, New York [etc.] Longmans, Green and Co., 1920), by Leonard Bairstow (page images at HathiTrust; US access only)
Post stall maneuvers and thrust vectoring performance analysis /, by L. Earl Miller, issuing body Air Force Wright Aeronautical Laboratories, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Asymptotic far field conditions for unsteady subsonic and transonic flows /, by Karl Gottfried Guderley, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Dayton. Research Institute (page images at HathiTrust)
Stability of a pair of stationary vortices in the leeward side of a cylinder in a potential flowfield /, by Shiva N. Singh, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Kentucky. Department of Mechanical Engineering (page images at HathiTrust)
Numerical study of separated turbulent flows /, by David C. Wilcox, issuing body Aerospace Research Laboratories (U.S.), and sponsor United States. National Technical Information Service (page images at HathiTrust)
Unsteady aerodynamics for advanced configurations., by M. T. Moore, L. V. Andrew, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
Aerodynamic testing in a free-flight spark range /, by G. L. Winchenbach, Air Force Wright Aeronautical Laboratories. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
Summary of instrumentation development and aerodynamic research in a hypersonic shock tunnel., by Charles E. Wittliff, Merle R. Wilson, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
Prediction of forces and moments on finned missiles at high angle of attack in transonic flow /, by William L. Oberkampf, United States. Air Force. Systems Command. sponsor, and Air Force Armament Laboratory. issuing body (page images at HathiTrust)
Unsteady aerodynamics for advanced configurations., by T. C. Li, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
Unsteady aerodynamics for advanced configurations., by E. R. Rodemich, L. V. Andrew, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
Energy-based design methodology for air vehicle systems : aerodynamic correlation study /, by Richard S. Figliola, Clemson University. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
Free-flight range tests of the MK76 MOD 5 Navy practice bobm at Mach numbers of 0.574 to 1.113 /, by G. L. Winchenback, Peter Daniels, Kenneth O. West, United States. Air Force. Systems Command. sponsor, and Air Force Armament Laboratory. issuing body (page images at HathiTrust)
STORESIM : an integrated system for multi-body cfd simulations using unstructured, adaptive grids /, by M. P. Reddy, Air Force Wright Aeronautical Laboratories. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
Unsteady aerodynamics for advanced configurations., by E. Albano, L. V. Andrew, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
Aerodynamic interference of wing-pylon-body combinations at low subsonic speeds /, by Kenneth Boland Walkley, Fred W. Martin, United States. Air Force. Systems Command. sponsor, Air Force Armament Laboratory. issuing body, and Auburn University. Department of Aerospace Engineering. sponsor (page images at HathiTrust)
Fluidic virtual aerosurfaces for flow control applications /, by Ari Glezer, George W. Woodruff School of Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
Parallel simulation of moving boundary flow using overset adaptive cartesian/prism grids and DES /, by Z. J. Wang, Michigan State University. Department of Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
Aerodynamic/dynamic interaction /, by Dean T. Mook, Ali Hasan Nayfeh, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Department. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
An experimental study of boattail pressures at high subsonic Mach numbers and high Reynolds numbers /, by John D. Lee, issuing body Aerospace Research Laboratories (U.S.), and sponsor Ohio State University. Research Foundation (page images at HathiTrust)
Interactive plotting of NASTRAN aerodynamic models using NPLOT and DISSPLA /, by Steven G. Harris and United States. Air Force. Air Force Weapons Laboratory. issuing body (page images at HathiTrust)
Computational methods for problems in aerodynamics using parallel and vector architecture /, by David Gottlieb, Brown University. Division of Applied Mathematics. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (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 /, by V. Zakkay, issuing body Aerospace Research Laboratories (U.S.), and sponsor New York University. Aerospace and Energetics Laboratory (page images at HathiTrust)
Subsonic flow of hot gas through a highly cooled constant-area channel /, by Harold Mirels, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)
Description and capabilities of the aeroballistic research facility /, by G. L. Winchenback, Judith Sullivan Kleist, D. G. Galanos, Billy Lucas, United States. Air Force. Systems Command. sponsor, and Air Force Armament Laboratory. issuing body (page images at HathiTrust)
Computational mechanics approach for multidisciplinary nonlinear sensitivity analysis /, by R. V. Grandhi, Wright State University. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
On the viscosity of dissociated air /, by F. K. Moore, United States. Air Force. Office of Scientific Research. issuing body, and Cornell Aeronautical Laboratory. sponsor (page images at HathiTrust)
The stability of compressible flows and transition through the speed of sound /, by John Pairman Brown and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
Turbulence modeling /, by John L. Lumley, Cornell University. Sibley School of Mechanical and Aerospace Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
Heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds / (Washington, D.C. : NACA, 1952), by Coleman duP. Donaldson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Technical note BN. (College Park.), by College Park. Institute for Fluid Dynamics and Applied Mathematics University of Maryland (page images at HathiTrust; US access only)
On the range of applicability of the transonic area rule / (Washington, D.C. : NACA, 1954), by John R. Spreiter, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)

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