Stability of airplanesSee also what's at your library, or elsewhere.
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Filed under: Stability of airplanes- Navigation aérienne et navigation sous-marine; deux faces d'un même problème ... (L. Geisler, 1910), by Henri Noalhat (page images at HathiTrust; US access only)
- Aeroplane design (R. M. McBride & co., 1917), by F. S. Barnwell and William H. Sayers (page images at HathiTrust)
- Théorie générale de l'action stabilisatrice des empennages horizontaux de l'aéroplane (H. Dunod et E. Pinat, 1913), by Georges de Bothezat (page images at HathiTrust; US access only)
- Aeroplanes in gusts. (E. & F. N. Spon;, 1913), by S. L. Walkden (page images at HathiTrust; US access only)
- Der schwebflug und die fallbewegung ebener tafeln in der luft. (L. Friederichsen & co., 1897), by Friedrich Ahlborn (page images at HathiTrust)
- Aerodonetics : constituting the second volume of a complete work on aerial flight (A. Constable, 1908), by F. W. Lanchester (page images at HathiTrust)
- Étude graphique et expérimental de la stabilité de l'aéroplane en air calme et en air agité (H. Dunod et E. Pinat, 1912), by Aristide Archille Delaunay (page images at HathiTrust; US access only)
- Stability in aviation : an introduction to dynamical stability as applied to the motions of aeroplanes (Macmillan, 1911), by G. H. Bryan (page images at HathiTrust)
- Die Stabilität der Flugzeuge : Einfuhrung in die dynamische Stabilität der Flugzeuge (J. Springer, 1914), by G. H. Bryan (page images at HathiTrust; US access only)
- La stabilisation automatique longitudinale des aéroplanes (Gauthier-Villars, 1912), by Adolphe Doutre (page images at HathiTrust; US access only)
- Étude de la stabilité de l'aéroplane (H. Dunof et E. Pinat, 1911), by Georges de Bothezat and Paul Painlevé (page images at HathiTrust; US access only)
- Les secrets du vol; les aéroplanes stabilisés; la sécurité dans le vol (Morice fréres, imprimeurs, 1928), by D Nault (page images at HathiTrust; US access only)
- Notes on dynamics for aerodynamicists. (Santa Monica, Calif., 1951), by Julius David Schetzer and inc. Douglas Aircraft Company (page images at HathiTrust)
- Die Stabilisierung der Flugzeuge (C.J.E. Volckmann nachf. G. m. b. H., 1917), by Carl Walther Vogelsang (page images at HathiTrust; US access only)
- Stabilité des aéroplanes; surface métacentrique (H. Dunod et É. Pinat, 1910), by Marcel Brillouin (page images at HathiTrust; US access only)
- USAF stability and control datcom (National Technical Information Service, 1975), by Douglas Aircraft Company, R. D. Finck, and D. E. Hoak (page images at HathiTrust)
- Aeroplane design (McBride, Nast & Co., 1916), by Frank Sowter Barnwell and William H. Sayers (page images at HathiTrust; US access only)
- Flying, the why and wherefore (The Aero, 1909), by Aero-Amateur (page images at HathiTrust; US access only)
- Use of an adaptive servo to obtain optimum airplane responses. (Cornell Aeronautical Laboratory, Inc., 1957), by Graham Campbell (page images at HathiTrust; US access only)
- The effects of atmospheric turbulence upon flight at low altitude and high speed. (Cornell Aeronautical Laboratory, inc., Flight Research Dept., 1961), by Charles Boris Notess (page images at HathiTrust)
- Proposed ground and flight check-out of variable L/D system installed in variable stability T-33 (Cornell Aeronautical Laboratory, inc., Buffalo, 1961), by Cornell Aeronautical Laboratory. Flight Research Dept and Charles Chalk (page images at HathiTrust)
- Flight evaluations of the effect of variable spiral damping in a JTB-26B airplane. (Cornell Aeronautical Laboratory, Inc., 1957), by Donald W. Rhoads (page images at HathiTrust)
- Development of a power-spectral gust design procedure for civil aircraft (Lockheed-California Co., 1966), by Frederic M Hoblit and United States. Federal Aviation Agency. Aviation Research and Development Service (page images at HathiTrust)
- Variable stability research aircraft. Submitted to the Panel on Acceleration Stress of the Armed Forces, National Research Council Committee on Bio-Astronautics, Woods Hole Conference, 16-24 July, 1959. ([Buffalo, N. Y., 1959), by Cornell Aeronautical Laboratory (page images at HathiTrust)
- Guidance and control/ACEE. (National Aeronautics and Space Administration :, 1981), by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Wind tunnel free flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Long P. Yip and Langley Research Center (page images at HathiTrust)
- Low speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Dana Morris Dunham and Langley Research Center (page images at HathiTrust)
- Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by David E. Reubush, Bobby L. Berrier, and Langley Research Center (page images at HathiTrust)
- Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Daniel G. Murri, Frank L. Jordan, and Langley Research Center (page images at HathiTrust)
- Flight characteristics of a modified Schweizer SGS 1-36 sailplane at low and very high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Alex G. Sim and Dryden Flight Research Facility (page images at HathiTrust)
- Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Francis J. Capone, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
- Investigation of the low subsonic flight characteristics of a model of a flat-top hypersonic-boost glide configuration having an arrowhead wing (National Aeronautics and Space Administration, 1959), by Peter C. Boisseau and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane (National Aeronautics and Space Administration, 1959), by Thomas W. Finch, Gene J. Matranga, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Analysis of an emergency deceleration and descent of the XB-70-1 airplane due to engine damage resulting from structural failure (National Aeronautics and Space Administration, 1966), by Chester H. Wolowicz and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Transonic aerodynamic damping and oscillatory stability in yaw and pitch for a model of a variable-sweep supersonic transport airplane (National Aeronautics and Space Administration ;, 1966), by Bruce R. Wright, Benjamin T. Averett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Description of an experimental (hydrogen peroxide) rocket system and its use in measuring aileron and rudder effectiveness of a light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Thomas C. O'Bryan, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
- Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Barrett L. Shrout, Roger H. Fournier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Informaton Office (page images at HathiTrust)
- Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Odell A. Morris, Crolyn B. Watson, Dennis E. Fuller, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- An Algorithm for maximum likelihood estimation using an efficient method for approximating sensitivities (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Patrick C. Murphy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Dale R. Satran and Langley Research Center (page images at HathiTrust)
- Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Zachary T. Applin, Paul L. Coe, and Langley Research Center (page images at HathiTrust)
- Wind-tunnel static and free-flight investigation of high-angle-of-attack stability and control characteristics of a model of the EA-6B airplane (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Frank L. Jordan, David E. Hahne, and Langley Research Center (page images at HathiTrust)
- Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45? (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by William P. Henderson, Laurence D. Leavitt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Dale R. Satran, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Aircraft ground tests and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Steven A. Johnson and Dryden Flight Research Facility (page images at HathiTrust)
- Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Peter F. Covell, Dorothy T. Howell, Ira J. Walker, and Langley Research Center (page images at HathiTrust)
- Stability of numerical integration techniques for transient rotor dynamic (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Albert F. Kascak and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Stability characteristics for a full-span model at Mach 0.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Robert R. Meyer, Langley Research Center, United States Air Force, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Flight-determined stability and control derivatives for the F-111 TACT research aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), by Alex G. Sim, Robert E. Curry, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Richmond P. Boyden, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
- Flight evaluation of the transonic stability and control charcteristics of an airplane incorporating a supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Neil W. Matheny, Donald H. Gatlin, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by George H. Neiner, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Improvement of maneuver aerodynamics by spanwise blowing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Gary E. Erickson and James F. Campbell (page images at HathiTrust)
- Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by David E. Hahne and Langley Research Center (page images at HathiTrust)
- Effects of control inputs on the estimation of stability and control parameters of a light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Robert L. Cannaday, William T. Suit, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- High-angle-of-attack stability characteristics of a three-surface fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Sue B. Grafton, Luat T. Nguyen, Mark A. Croom, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James L. Dillon, Jimmy L. Pittman, Langley 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 number 0.2 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Jim A. Penland, James L. Dillon, Theodore R. Creel, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Ames Research Center, Richard F. Vomaske, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- A comparison of the V/STOL handling qualities of the VAK-191B with requirements of AGARD report 577 and MIL-F-83300 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Seth B. Anderson, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Pseudosteady-state analysis of nonlinear aircraft maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by John W. Young, Katherine G. Johnson, Albert A. Schy, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by A. Warner Robins, David S. Miller, Milton Lamb, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
- Low-speed wind-tunnel tests of an advanced eight-bladed propeller (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Paul L. Coe, Dana Morris Dunham, Garl L. Gentry, and Langley Research Center (page images at HathiTrust)
- Simulator study of vortex encounters by a twin-engine, commercial, jet transport airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Earl C. Hastings, Gerald L. Keyser, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Determination of airplane model structure from flight data using splines and stepwise regression (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Vladislav Klein, James G. Batterson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Steven M. Sliwa, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Investigation of Northrop F-5A wing buffet intensity in transonic flight (National Aeronautics and Space Administration ;, 1974), by Chintsun Hwang, W. S. Pi, Ames Research Center, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
- Characterization of nongaussian atmospheric turbulence for prediction of aircraft response statistics (National Aeronautics and Space Administration ;, 1977), by William D. Mark 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. Volume III, Propulsion subsystems, performance, stability and control, propellers, and flight safety (National Aeronautics and Space Administration ;, 1970), by Clifford J. Moore, Dennis M. Phillips, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
- Riding and handling qualities of light aircraft : a review and analysis (National Aeronautics and Space Administration, 1972), by Frederick O. Smetana, W. Donald Johnson, Delbert C. Summey, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
- Study of load alleviation and mode suppression (LAMS) on the YF-12A airplane (National Aeronautics and Space Administration ;, 1972), by Lester D. Edinger, Alan R. Curtis, Frederick L. Schenk, Flight Research Center (U.S.), Honeywell Inc, and Lockheed Aircraft Corporation (page images at HathiTrust)
- Investigation of steady and fluctuating pressures associated with the transonic buffeting and wing rock of a one-seventh scale model of the F-5A aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Chintsun Hwang, W. S. Pi, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Ames Research Center, and Northrop Corporation (page images at HathiTrust)
- Investigations of simulated aircraft flight through thunderstorm outflows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Walter Frost and George C. Marshall Space Flight Center (page images at HathiTrust)
- Pilot evaluation of sailplane handling qualities (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by A. G. Bennett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Investigation, development, and application of optimal output feedback theory. Volume III, The relationship between dynamic compensators and observers and Kalman Filters (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by John R. Broussard and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
- Stability and control of the Gossamer human-powered aircraft by analysis and flight test (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Henry R. Jex, David G. Mitchell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, inc Systems Technology, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
- A Study of the application of singular perturbation theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Raman K. Mehra, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- A model-based technique for predicting pilot opinion ratings for large commercial transporters (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by William H. Levison, Beranek Bolt, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
- Calculation of aerodynamic characteristics of airplane configurations at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Jing-Biau Tseng, C. Edward Lan, and Langley Research Center (page images at HathiTrust)
- Effect of vertical-tail location on the aerodynamic characteristics at subsonic speeds of a close-coupled canard configuration (National Aeronautics and Space Administration ;, 1975), by Jarrett K. Huffman and Langley Research Center (page images at HathiTrust)
- L'équilibre des aéroplanes ... (F. L. Vivien, 1910), by Robert Desmons (page images at HathiTrust; US access only)
- NASA TN D-3970 (National Aeronautics and Space Administration ;, 1967), by Norman R. Driscoll, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8 scale F-15 airplane model obtained from flight test (National Aeronautics and Space Administration ;, 1976), by Kenneth W. Iliff, Mary F. Shafer, Richard E. Maine, and Flight Research Center (U.S.) (page images at HathiTrust)
- The effect of winglets on the static aerodynamic stability characteristics of a representative second generation jet transport model (U.S. National Aeronautics and Space Administration ;, 1976), by Peter F. Jacobs, Stuart G. Flechner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 (National Aeronautics and Space Administration ;, 1977), by Richard J. Re, Francis J. Capone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport (National Aeronautics and Space Administration :, 1970), by Joseph R. Chambers, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- NASA TN D-6629 (National Aeronautics and Space Administration :, 1972), by William B. Kemp, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5409 (National Aeronautics and Space Administration :, 1969), by Joseph R. Chambers, Ernie L. Anglin, James S. Bowman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-6656 (National Aeronautics and Space Administration :, 1972), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Flight-determined derivatives and dynamic characteristics of the CV-990 airplane (National Aeronautics and Space Administration ;, 1972), by Glenn B. Gilyard and Flight Research Center (U.S.) (page images at HathiTrust)
- Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 (National Aeronautics and Space Administration :, 1971), by Walter P. Nelms, Charles L. Thomas, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- An analysis of the limit-cycle and structural-resonance characteristics of the X-15 stability augmentation system (National Aeronautics and Space Administration, 1967), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio (National Aeronautics and Space Administration ;, 1968), by Patrick J. Johnston, Robert D. Witcofski, and Langley Research Center (page images at HathiTrust)
- Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 (National Aeronautics and Space Administration, 1960), by Victor L. Peterson, Loren G. Bright, and Ames Research Center (page images at HathiTrust)
- Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration (National Aeronautics and Space Administration, 1959), by William J. Alford, William P. Handerson, Arvo A. Luoma, and Langley Research Center (page images at HathiTrust)
- Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers (National Aeronautics and Space Administration ;, 1972), by Larry W. Strutz and Flight Research Center (U.S.) (page images at HathiTrust)
- Evaluation of effects of high-altitude turbulence encounters on the XB-70 airplane (National Aeronautics and Space Administration, 1971), by Ronald J. Wilson, Richard R. Larson, Betty J. Love, Flight Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Dynamic stability derivatives of a jet transport configuration with high thrust-weight ratio and an externally blown jet flap (National Aeronautics and Space Administration ;, 1971), by Sue B. Grafton, Charles C. Smith, Lysle P. Parlett, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Comparison of several methods for estimating low-speed stability derivatives for two airplane configurations (National Aeronautics and Space Administration ;, 1971), by Herman S. Fletcher, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Effect of engine position and high-lift devices on aerodynamic characteristics of an external-flow jet-flap STOL model (National Aeronautics and Space Administration ;, 1971), by Charles C. Smith, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Maneuver and buffet characteristics of fighter aircraft (National Aeronautics and Space Administration ;, 1973), by Edward J. Ray, Julian G. Carmichael, Linwood W. McKinney, and Langley Research Center (page images at HathiTrust)
- Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75° (National Aeronautics and Space Administration, 1959), by M. Leroy Spearman, Gerald V. Foster, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 degree delta wing (National Aeronautics and Space Administration, 1960), by Cornelius Driver, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Stability and control characteristics of a large-scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio (National Aeronautics and Space Administration, 1971), by V. Robert Page, Thomas N. Aiken, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
- Stability and control characteristics at a Mach number of 1.97 of an airplane configuration having two types of variable- sweep wings (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)
- The effects of wing-tip droop on the aerodynamic characteristics of a delta-wing aircraft at supersonic speeds (National Aeronautics and Space Administration, 1960), by Richard H. Peterson and Ames Research Center (page images at HathiTrust)
- Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model (National Aeronautics and Space Administration ;, 1973), by James L. Thomas, Delwin R. Croom, Danny R. Hoad, and Langley Research Center (page images at HathiTrust)
- Flight evaluation of advanced control systems and displays on a general aviation airplane (National Aeronautics and Space Administration ;, 1974), by Paul C. Loschke and Flight Research Center (U.S.) (page images at HathiTrust)
- Monte Carlo analysis of inaccuracies in estimated aircraft parameters caused by unmodeled flight instrumentation errors (National Aeronautics and Space Administration ;, 1975), by Ward F. Hodge, Wayne H. Bryant, and Langley Research Center (page images at HathiTrust)
- Low-speed wind-tunnel investigation of a large-scale advanced arrow-wing supersonic transport configuration with engines mounted above wings for upper-surface blowing (National Aeronautics and Space Administration :, 1976), by James P. Shivers, Paul L. Coe, H. Clyde McLemore, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NACA wartime reports (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)
- Report on the special field "interference" to the wind tunnel committee in February 1945 (National Advisory Commitee for Aeronautics ;, 1953), by Hermann Schlichting and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
- Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model (National Advisory Committee for Aeronautics, 1957), by Powell M. Lovell, Lysle P. Parlett, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Some recent research on the handling qualities of airplanes (National Advisory Committee for Aeronautics, 1956), by Walter C. Williams, William H. Phillips, Flight Research Center (U.S.), United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds (National Advisory Committee for Aeronautics, 1952), by Paul E. Purser, Jesse L. Mitchell, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The use of the horizontal tail for roll control (National Advisory Committee for Aeronautics, 1956), by John P. Campbell and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2©� delta wing and an unswept horizontal tail. (National Advisory Committee for Aeronautics, 1958), by Alan B. Kehlet, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Effect of some present-day airplane design trends on requirements for lateral stability (National Advisory Committee for Aeronautics ;, 1941), by M. J. Bamber and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Approximate corrections for the effects of compressibility on the subsonic stability derivatives of swept wings (National Advisory Committee for Aeronautics, 1949), by Lewis R. Fisher and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot (National Advisory Committee for Aeronautics, 1949), by Robert T. Jones, Leonard Sternfield, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane (National Advisory Committee for Aeronautics, 1949), by Charles J. Liddell, Donovan R. Heinle, Rudolph D. Van Dyke, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A survey of stability analysis techniques for automatically controlled aircraft (National Advisory Committee for Aeronautics, 1951), by Arthur L. Jones, Benjamin R. Briggs, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Analysis of the effects of wing interference on the tail contributions to the rolling derivatives (National Advisory Committee for Aeronautics, 1951), by William H. Michael and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A least squares curve fitting method with applications to the calculation of stability coefficients from transient-response data (National Advisory Committee for Aeronautics, 1951), by Marvin Shinbrot and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effect of vertical-tail area and length on the yawing stability characteristics of a model having a 45©� sweptback wing (National Advisory Committee for Aeronautics, 1951), by William Letko and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw (National Advisory Committee for Aeronautics, 1952), by John D. Bird, Sadie M. Hubbard, Lewis R. Fisher, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip (National Advisory Committee for Aeronautics, 1953), by Donald R. Riley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model (National Advisory Committee for Aeronautics, 1954), by Alex Goodman, David F. Thomas, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A wind-tunnel test technique for measuring the dynamic rotary stability derivatives including the cross derivatives at high Mach numbers (National Advisory Committee for Aeronautics, 1955), by Benjamin H. Beam and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° (National Aeronautics and Space Administration, 1960), by Gerald V. Foster and United States National Aeronautics and Space Administration (page images at HathiTrust)
- A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations (National Aeronautics and Space Administration, 1960), by Ralph P. Bielat, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Stability and control characteristics at a mach number of 2.01 of a supersonic VTOL airplane model having a broad fuselage and small delta wings (National Aeronautics and Space Administration, 1961), by Cornelius Driver, M. Leroy Spearman, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Subsonic flight tests of a 1/7-scale radio-controlled model of the North American X-15 airplane with particular reference to high angle-of-attack conditions (National Aeronautics and Space Administration, 1960), by Donald E. Hewes, James L. Hassell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration (National Aeronautics and Space Administration, 1960), by James L. Hassell and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 (National Aeronautics and Space Administration, 1959), by Cornelius Driver, M. Leroy Spearman, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes (National Aeronautics and Space Administration, 1960), by James L. Hassell, Donald E. Hewes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Effect of configuration variables on the subsonic longitudinal stability characteristics of a high-tail transport configuration (National Aeronautics and Space Administration ;, 1965), by Edward J. Ray, Robert T. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Free-flight investigation at supersonic speeds of the stability and drag of a 79° clipped delta boost-glide configuration including an analog study of coupled motions during the flight (National Aeronautics and Space Administration, 1961), by Sherwood Hoffman, Willard S. Blanchard, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Simulation study of a high-performance aircraft including the effect on pilot control of large accelerations during exit and reentry flight (National Advisory Committee for Aeronautics, 1958), by Robert E. Andrews, Robert A. Champine, James B. Whitten, C. H. Woodling, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- The Behavior of conventional airplanes in situations thought to lead to most crashes (National Advisory Committee for Aeronautics ;, 1931), by Fred E. Weick and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Influence of large amounts of wing sweep on stability and control problems of aircraft (National Advisory Committee for Aeronautics ;, 1946), by Hartley A. Soule and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat (National Advisory Committee for Aeronautics, 1948), by Roland E. Olson, Norman S. Land, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Stability derivatives of triangular wings at supersonic speeds (National Advisory Committee for Aeronautics, 1948), by H. S. Ribner, Frank S. Malvestuto, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Flight measurements of the flying qualities of five light airplanes (National Advisory Committee for Aeronautics, 1948), by Paul A. Hunter and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1944), by Harry J. Goett, Noel K. Delany, Ames Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryanksy, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by Isidore G. Recant, Arthur R. Wallace, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), by John W. McKee, Robert B. Liddell, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by John G. Lowry, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by John G. Lowry, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by Isidore G. Recant, Robert S. Swanson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Equilibre, centrage et classification des aéroplanes. (Librairie aéronautique, 1910), by Raymond Saulnier (page images at HathiTrust; US access only)
- Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds, transonic-bump method (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), by Harold S. Johnson, William C. Hayes, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Theoretical investigation of some discontinuous yaw dampers (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), by William H. Phillips, Helmut A. Kuehnel, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Low-speed static stability characteristics of a cambered-delta-wing model (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), by John M. Riebe, William C. Moseley, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Notes on the static longitudinal stability and control of aircraft. (Flight Research Dept., Cornell Aeronautical Laboratory, 1953), by Waldemar Otto Brehaus (page images at HathiTrust; US access only)
- Collected papers on instability of shell structures, 1962. (National Aeronautics and Space Administration, 1962), by NASA Symposium on Instability of Shell Structures (1962 : Langley Research Center), United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Unsteady supersonic flow (Headquarters, Air Research and Development Command, 1955), by John W. Miles and United States. Air Force. Air Research and Development Command (page images at HathiTrust; US access only)
- Structural response to discrete and continuous gusts of an airplane having wing-bending flexibility and a correlation of calculated and flight results (U.S. Government Printing Office, 1954), by John C. Houbolt, Eldon E. Kordes, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Analytical sensor redundancy assessment (FAA Technical Center ;, 1988), by D. B. Mulcare, M. K. Smith, L. E. Downing, Federal Aviation Administration Technical Center (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
- Final report on extraction of aircraft stability coefficients from flight test data and theoretical and experimental studies on selected problems of high speed aerodynamics and dynamic stability (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by Lloyd E. Wilkie, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
- Effect of boundary layer control on airplane stability and control as determined by flight test : final report (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by Cessna Aircraft Company, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and United States. Wright Air Development Division (page images at HathiTrust)
- Étude de la stabilité de l'aéroplane ... (H. Dunod et E. Pinat, 1911), by Georges de Bothezat and Paul Painlevé (page images at HathiTrust; US access only)
- Fixed-base simulator investigation of the effects of L [alpha] and true speed on pilot opinion of longitudinal flying qualities (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963., 1963), by Charles R. Chalk, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
- Predictive methods for the dynamic response of a quad tilt-duct V/STOL aircraft in transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by Irving Carl Statler, A. Sowyrda, J. C. Erickson, G. Kurylowich, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
- Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by Frederick D. Newell, Cornell Aeronautical Laboratory, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Man-machine tracking performance with short-period oscillatory control system transients (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Frederick A. Muckler, United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and University of Illinois (Urbana-Champaign campus). Aviation Research Laboratory (page images at HathiTrust)
- Development and flight calibration of a variable-drag device on a variable stability T-33 airplane (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Frederick D. Newell, Arno E. Schelhorn, B. H. Dolbin, Wright-Patterson Air Force Base (Ohio), Cornell Aeronautical Laboratory, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Validation of United States Air Force stability and control Datcom methodologies for straight-tapered sweptforward wings (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Daniel G. Sharpes, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
- Lateral handling quality requirements from airframe-human pilot system studies (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Irving L. Ashkenas, Duane T. McRuer, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
- An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by T. O. Shadow, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Static stability and drag characteristics of a hypersonic aircraft design at Mach numbers 1.5 to 5.6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), by J. T. Jr Best, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Aircraft motion sensitivity to cross and cross-coupling damping derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by R. W. Butler, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- An experimental study of passive control of hypersonic cavity flow oscillations (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Aerospace Sciences, 1998., 1998), by D. S. Dolling, Y. L. Leu, S. W. Perng, University of Texas at Austin. Department of Aerospace Engineering and Engineering Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
- Select means for determining unsteady aerodynamic response characteristics from static data (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2000., 2000), by Gregory A. Addington and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
- Research on hypersonic stability problems (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, United States Air Force, 1974., 1974), by O. Walchner, Aerospace Research Laboratories (U.S.), and United States. Air Force. Office of Aerospace Research (page images at HathiTrust)
- Control-surface deflection effects on the innovative control effectors (ICE 101) design (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2000., 2000), by Gregory A. Addington and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
- Aerodynamic analysis for the design environment (AANDE). Volume 2, User's manual (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 1999., 1999), by M. H. Love, D. D. Egle, Lockheed Martin. Tactical Aircraft Systems, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
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