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Stability of airplanes

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• Aerodynamics
• Aeronautics
• Flight
• Airplanes

• Airplanes -- Handling characteristics
• Stability of airplanes, Lateral
• Stability of airplanes, Longitudinal

• Airplanes -- Stability

• Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 / (Washington, D.C. : National Aeronautics and Space Administration, [1959]), by David E. Fetterman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aeroplane design, (London, McBride, Nast & Co., 1916), by Frank Sowter Barnwell and William H. Sayers (page images at HathiTrust; US access only)
• Pilot evaluation of sailplane handling qualities / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• Use of an adaptive servo to obtain optimum airplane responses. (Buffalo, Cornell Aeronautical Laboratory, Inc., 1957), by Graham Campbell (page images at HathiTrust; US access only)
• 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)
• Stability of numerical integration techniques for transient rotor dynamic / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Albert F. Kascak 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 / (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 Seth B. Anderson, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Collected papers on instability of shell structures, 1962. (Washington, 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)
• Ground and flight test methods for determining limit cycle and structural resonance characteristics of aircraft stability augmentation systems / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1972), by Weneth D. Painter, George J. Sitterle, and Flight Research Center (U.S.) (page images at HathiTrust)
• Effect of winglets on a first-generation jet transport wing. (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 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)
• Aircraft ground tests and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes / (Washington, D.C. : 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)
• 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° / (Washington [D.C.] : 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 / (Washington [D.C.] : 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)
• Effect of control surface mass unbalance on the stability of a closed-loop active control system / (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 E. Nissim and Dryden Flight Research Facility (page images at HathiTrust)
• 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 / (Washington [D.C.] : 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 / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by James L. Hassell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of load alleviation and mode suppression (LAMS) on the YF-12A airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
• Effect of vertical-tail location on the aerodynamic characteristics at subsonic speeds of a close-coupled canard configuration / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Jarrett K. Huffman 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Larry W. Strutz and Flight Research Center (U.S.) (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 / (Washington [D.C.] : 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 / (Washington [D.C.] : 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 / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Bruce R. Wright, Benjamin T. Averett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• 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 / (Washington [D.C.] : 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Edward J. Ray, Robert T. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds / (Washington, [DC] : National Aeronautics and Space Administration, [1963]), by Robert S. Osborne, George M. Ware, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Riding and handling qualities of light aircraft : a review and analysis / (Washington : 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)
• Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by David E. Stepner, Raman K. Mehra, Langley Research Center, and inc Systems Control (page images at HathiTrust)
• Flight testing techniques for the evaluation of light aircraft stability derivitives : a review and analysis / (Washington : National Aeronautics and Space Administration, 1972), by Frederick O. Smetana, W. Donald Johnson, Delbert C. Summey, Langley Research Center, United States National Aeronautics and Space Administration, and North Carolina State University (page images at HathiTrust)
• Effects of time-shifted data on flight-determined stability and control derivatives / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Sandra Thornberry Steers, Kenneth W. Iliff, and Flight Research Center (U.S.) (page images at HathiTrust)
• A FORTRAN program for determining aircraft stability and control derivatives from flight data / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Richard E. Maine, Kenneth W. Iliff, and Flight Research Center (U.S.) (page images at HathiTrust)
• Flight characteristics of a modified Schweizer SGS 1-36 sailplane at low and very 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 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 / (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 Francis J. Capone, Mary L. Mason, and Langley Research Center (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 Clifford J. Moore, Dennis M. Phillips, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Effects of a simple stability augmentation system on the performance of non-instrument-qualified light-aircraft pilots during instrument flight / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Norman R. Driscoll, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Randall D. Grove 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)
• Maneuver and buffet characteristics of fighter aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Edward J. Ray, Julian G. Carmichael, Linwood W. McKinney, and Langley Research Center (page images at HathiTrust)
• Flight evaluation of advanced control systems and displays on a general aviation airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Ward F. Hodge, Wayne H. Bryant, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by Kenneth W. Iliff, Mary F. Shafer, Richard E. Maine, and Flight Research Center (U.S.) (page images at HathiTrust)
• Flight-determined derivatives and dynamic characteristics of the CV-990 airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Glenn B. Gilyard and Flight Research Center (U.S.) (page images at HathiTrust)
• Guidance and control/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)
• Investigation, development, and application of optimal output feedback theory. (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 John R. Broussard and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (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)
• Unsteady supersonic flow / (Baltimore, Md. : 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)
• Development of a power-spectral gust design procedure for civil aircraft / (Burbank, Calif. : Lockheed-California Co., 1966), by Frederic M Hoblit and United States. Federal Aviation Agency. Aviation Research and Development Service (page images at HathiTrust)
• Bibliography of Supersonic Cruise Research (SCR) Program from 1980 to 1983 / (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 Sherwood Hoffman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Structural response to discrete and continuous gusts of an airplane having wing-bending flexibility and a correlation of calculated and flight results / (Washington, D.C. : 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)
• Flying, the why and wherefore / (London : The Aero, [1909?]), by Aero-Amateur (page images at HathiTrust; US access only)
• Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• Analytical sensor redundancy assessment / (Atlantic City International Airport, N.J. : FAA Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [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)
• 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)
• Notes on the static longitudinal stability and control of aircraft. (Buffalo, N. Y. : Flight Research Dept., Cornell Aeronautical Laboratory, 1953), by Waldemar Otto Brehaus (page images at HathiTrust; US access only)
• Light airplane crash tests at three pitch angles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service], 1979), by Victor L. Vaughan, Emilio Alfaro-Bou, Langley Research Center, 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)
• 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)
• Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (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)
• User's manual for LINEAR, a FORTRAN program to derive linear aircraft models / (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 Eugene L. Duke, Robert F. Antoniewicz, Brian P. Patterson, and Dryden Flight Research Facility (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)
• Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing / (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 Daniel G. Murri, Frank L. Jordan, and Langley Research Center (page images at HathiTrust)
• SPINEQ, a program for determining aircraft equilibrium spin characteristics including stability / (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 William M. Adams 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• Airplane stability calculations with a card programmable pocket calculator / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Windsor L. Sherman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration / (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 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 / (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 Zachary T. Applin, Paul L. Coe, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration / (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 Daniel G. Murri, Sue B. Grafton, Luat T. Nguyen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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 / (Washington, D.C. : 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?/ (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 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)
• Estimation of airplane stability and control derivatives from large amplitude longitudinal maneuvers / (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 James G. Batterson, 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 / (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 Dale R. Satran, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 / (Washington, D.C. : 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)
• Flight-determined stability and control derivatives for the F-111 TACT research aircraft / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Service ; Springfield, Va. : For sale by the National 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)
• Determination of stability and control parameters of a light airplane from flight data using two estimation methods / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Vladislav Klein, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (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)
• 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)
• Low-speed static and dynamic force tests of a generic supersonic cruise fighter 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, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (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 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)
• Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration / (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 Sue B. Grafton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Low-speed wind-tunnel tests of an advanced eight-bladed propeller / (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 L. Coe, Dana Morris Dunham, Garl L. Gentry, and Langley Research Center (page images at HathiTrust)
• Preliminary design study of a lateral-directional control system using thrust vectoring / (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 Frederick J. Lallman and Langley Research Center (page images at HathiTrust)
• Similitude requirements and scaling relationships as applied to model testing / (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 Chester H. Wolowicz, William P. Gilbert, James S. Bowman, Langley Research Center, Hugh L. Dryden Flight 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 by using modified stepwise regression / /c Vladislav Klein, James G. Batterson and Patrick C. Murphy. (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 Vladislav Klein, Patrick C. Murphy, James G. Batterson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Simulator study of vortex encounters by a twin-engine, commercial, jet transport airplane / (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 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 / (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 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 / (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)
• Study of stability of large maneuvers of airplanes / (Washington, D.C. : National Aeronautics and Space Administration, 1974), by Emile K. Haddad, Lockheed-Georgia Company, and Langley Research Center (page images at HathiTrust)
• Input design for identification of aircraft stability and control derivatives / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Narendra K. Gupta, W. Earl Hall, Flight Research Center (U.S.), and inc Systems Control (page images at HathiTrust)
• Characterization of nongaussian atmospheric turbulence for prediction of aircraft response statistics / ([Washington] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by William D. Mark and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Control definition study for advanced vehicles / (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 Maris Lapins, Grumman Aerospace Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stability and control of the Gossamer human-powered aircraft by analysis and flight test / (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 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)
• Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 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 / (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)
• Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [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 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Victor L. Peterson, Loren G. Bright, and Ames Research Center (page images at HathiTrust)
• Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Barbara J. Sort, Simon C. Sommer, and Ames Research Center (page images at HathiTrust)
• Evaluation of effects of high-altitude turbulence encounters on the XB-70 airplane / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
• Evaluation of turbulence reduction devices for the Langley 8-foot Transonic Pressure Tunnel / (Washington, D.C. : National Aeronautics and Space Administration, 1981), by Marion O. McKinney, James Scheiman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Gerald V. Foster, 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 variable-wing-sweep configuration with outboard wing panels swept back 75° / (Washington, [D.C.] : 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° delta wing / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Cornelius Driver, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Louis F. Vosteen and Langley Research Center (page images at HathiTrust)
• Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Norman H. Silvers, Jane S. Wills, Julia A. Lancaster, and Langley 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 / (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)
• The effects of wing-tip droop on the aerodynamic characteristics of a delta-wing aircraft at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Richard H. Peterson and Ames Research Center (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 / (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 Thomas C. O'Bryan, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Programmer'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], 1981), by Richard E. Maine, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An Algorithm for maximum likelihood estimation using an efficient method for approximating sensitivities / (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 Patrick C. Murphy 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• Pseudosteady-state analysis of nonlinear aircraft maneuvers / (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 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 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National 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)
• Computer mechanization of six-degree of freedom flight equations / ([Washington, D.C.] : National Aeronautics and Space Administration, [1969]), by L. E. Fogarty and R. M. Howe (page images at HathiTrust)
• Investigation of Northrop F-5A wing buffet intensity in transonic flight / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Chintsun Hwang, W. S. Pi, Ames Research Center, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Stability and control of maneuvering high-performance aircraft / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Robert F. Stengel, Paul W. Berry, Analytic Sciences Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pogo suppression on space shuttle : early studies / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Stanley G. Rubin, J. G. Payne, W. G. Wagner, Langley Research Center, and Aerospace Corporation (page images at HathiTrust)
• A Study of the application of singular perturbation theory / (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 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 / (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 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 / (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)
• The airplane as an object of control : block diagrams of the equations of perturbed airplane motion / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by V. S. Vedrov, V. N. Surina, and G. L. Romanov (page images at HathiTrust)
• An analytical study of turbulence responses, including horizontal-tail loads, of a control-configured vehicle with relaxed static stability / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Boyd Perry and Langley Research Center (page images at HathiTrust)
• The effect of winglets on the static aerodynamic stability characteristics of a representative second generation jet transport model / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970), by Joseph R. Chambers, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Definition and application of longitudinal stability derivatives for elastic airplanes / (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 B. Kemp, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 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)
• A wind-tunnel evaluation of analytical techniques for predicting static stability and control characteristics of flexible 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 Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of several methods for estimating low-speed stability derivatives for two airplane configurations / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Herman S. Fletcher, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Collected papers on instability of shell structure, 1962 / (Washington : 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)
• 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)
• Stability and control characteristics of a large-scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio / (Washington, D.C. : 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)
• Low-speed wind-tunnel investigation of a large-scale advanced arrow-wing supersonic transport configuration with engines mounted above wings for upper-surface blowing / (Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1976), by James P. Shivers, Paul L. Coe, H. Clyde McLemore, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stabilité des aéroplanes; surface métacentrique, (Paris, H. Dunod et É. Pinat, 1910), by Marcel Brillouin (page images at HathiTrust; US access only)
• Equilibre, centrage et classification des aéroplanes. (Paris, Librairie aéronautique, 1910), by Raymond Saulnier (page images at HathiTrust; US access only)
• Aeroplanes in gusts. (London, E. & F. N. Spon;, 1913), by S. L. Walkden (page images at HathiTrust; US access only)
• La stabilisation automatique longitudinale des aéroplanes; (Paris, Gauthier-Villars, 1912), by Adolphe Doutre (page images at HathiTrust; US access only)
• Navigation aérienne et navigation sous-marine; deux faces d'un même problème ... (Paris, L. Geisler, 1910), by Henri Noalhat (page images at HathiTrust; US access only)
• Die Stabilität der Flugzeuge : Einfuhrung in die dynamische Stabilität der Flugzeuge / (Berlin : J. Springer, 1914), by G. H. Bryan (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, (Berlin-Charlottenburg, C.J.E. Volckmann nachf. G. m. b. H., 1917), by Carl Walther Vogelsang (page images at HathiTrust; US access only)
• 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)
• Étude de la stabilité de l'aéroplane (Paris, H. Dunof et E. Pinat, 1911), by Georges de Bothezat and Paul Painlevé (page images at HathiTrust; US access only)
• Aerodonetics : constituting the second volume of a complete work on aerial flight / (London : 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; (Paris, H. Dunod et E. Pinat, 1912), by Aristide Archille Delaunay (page images at HathiTrust; US access only)
• USAF stability and control datcom / (Springfield, Va. : National Technical Information Service, 1975?), by Douglas Aircraft Company, R. D. Finck, and D. E. Hoak (page images at HathiTrust)
• Effect of boundary layer control on airplane stability and control as determined by flight test : final report /, by originator Cessna Aircraft Company, United States. Air Force. Air Research and Development Command. sponsor, Wright Air Development Center issuing body, and United States. Wright Air Development Division. WACD technical report (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)
• Investigation of phygoid effects on GCA landings /, by Fred Newell, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (page images at HathiTrust)
• Some recent research on the handling qualities of airplanes / (Washington, D.C. : 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. NACA research memorandum, 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. / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Alan B. Kehlet, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Simulation study of a high-performance aircraft including the effect on pilot control of large accelerations during exit and reentry flight / (Washington, D.C. : 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. NACA research memorandum (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 / (Washington, D.C. : 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)
• Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model / (Washington : 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)
• Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Paul E. Purser, Jesse L. Mitchell, 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)
• The use of the horizontal tail for roll control / (Washington, [D.C.] : National Advisory Committee for Aeronautics, [1956]), by John P. Campbell and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of some present-day airplane design trends on requirements for lateral stability / (Washington D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (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)
• Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model / (Washington, D.C. : 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1955]), by Benjamin H. Beam and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The Behavior of conventional airplanes in situations thought to lead to most crashes / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1931), by Fred E. Weick and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Predictive methods for the dynamic response of a quad tilt-duct V/STOL aircraft in transition /, by Irving Carl Statler, A. Sowyrda, J. C. Erickson, G. Kurylowich, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
• Man-machine tracking performance with short-period oscillatory control system transients /, by Frederick A. Muckler, sponsor United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command. issuing body, and sponsor University of Illinois (Urbana-Champaign campus). Aviation Research Laboratory (page images at HathiTrust)
• Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities /, by Frederick D. Newell, sponsor Cornell Aeronautical Laboratory, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Report on the special field "interference" to the wind tunnel committee in February 1945 / (Washington, D.C. : National Advisory Commitee for Aeronautics ;, [1953]), by Hermann Schlichting and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Aircraft weight and balance handbook. ([Oklahoma City, OK] : U.S. Dept. of Transportation, Federal Aviation Administration, Flight Standards Service, 1999), by United States. Federal Aviation Administration. Office of Flight Standards (page images at HathiTrust)
• Théorie générale de l'action stabilisatrice des empennages horizontaux de l'aéroplane, (Paris, H. Dunod et E. Pinat, 1913), by Georges de Bothezat (page images at HathiTrust; US access only)
• Measurement of the longitudinal moment of inertia of a flexible airplane / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Henry Ambrose Jr Cole, Frances L. Bennion, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Effect of tilt on the propeller axis on the longitudinal-stability characteristics of single-engine airplanes / (Washington, D.C. : 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)
• L'équilibre des aéroplanes ... (Paris, F. L. Vivien, 1910), by Robert Desmons (page images at HathiTrust; US access only)
• Aeroplane design, (New York, R. M. McBride & co., 1917), by F. S. Barnwell and William H. Sayers (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)
• Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane / (Washington, D.C. : 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)
• Wind tunnel investigation of effect of yaw on lateral-stability characteristics. 4 - Symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail / (Washington, D.C. : 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)
• Wind-tunnel investigation of a revised horizontal tail surface for the Grumman TBF-1 airplane / (Washington, D.C. : 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)
• Charts showing stability and control characteristics of airplanes in flight / (Washington, D.C. : National Advisory Committee for Aeronautics, [1944]), by Langley Aeronautical Laboratory and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps / (Washington, D.C. : 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)
• Additional power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps / (Washington, D.C. : 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)
• Determination of the stability and control characteristics of airplanes from tests of powered models / (Washington, D.C. : 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)
• Low-speed static stability characteristics of a cambered-delta-wing model /, by John M. Riebe, William C. Moseley, Langley Aeronautical Laboratory, 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 / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1946), by Hartley A. Soule and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Stability derivatives of triangular wings at supersonic speeds / (Washington, D.C. : 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)
• 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 /, 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 /, by William H. Phillips, Helmut A. Kuehnel, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Fixed-base simulator investigation of the effects of L [alpha] and true speed on pilot opinion of longitudinal flying qualities /, by Charles R. Chalk, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
• Validation of USAF stability and control Datcom methodologies for straight-tapered sweptforward wings /, by Daniel G. Sharpes, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• The determination of lateral handling quality requirements from airframe-human pilot system studies /, by Irving L. Ashkenas, Duane T. McRuer, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Development and flight calibration of a variable-drag device on a variable stability T-33 airplane /, by Frederick D. Newell, Arno E. Schelhorn, B. H. Dolbin, sposnor Wright-Patterson Air Force Base (Ohio), sponsor Cornell Aeronautical Laboratory, and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• The effects of atmospheric turbulence upon flight at low altitude and high speed. (Buffalo, 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 ([Buffalo] 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. (Buffalo, Cornell Aeronautical Laboratory, Inc., 1957), by Donald W. Rhoads (page images at HathiTrust)
• An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers /, by T. O. Shadow, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Aircraft motion sensitivity to cross and cross-coupling damping derivatives /, by R. W. Butler, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• An experimental study of passive control of hypersonic cavity flow oscillations /, by D. S. Dolling, Y. L. Leu, S. W. Perng, sponsor University of Texas at Austin. Department of Aerospace Engineering and Engineering Mechanics, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Control-surface deflection effects on the innovative control effectors (ICE 101) design /, 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)., 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)
• Select means for determining unsteady aerodynamic response characteristics from static data /, by Gregory A. Addington and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Static stability and drag characteristics of a hypersonic aircraft design at Mach numbers 1.5 to 5.6 /, by J. T. Jr Best, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Research on hypersonic stability problems /, by O. Walchner, issuing body Aerospace Research Laboratories (U.S.), and United States. Air Force. Office of Aerospace Research (page images at HathiTrust)
• Étude de la stabilité de l'aéroplane ... (Paris : H. Dunod et E. Pinat, 1911), by Georges de Bothezat and Paul Painlevé (page images at HathiTrust; US access only)
• Stability in aviation : an introduction to dynamical stability as applied to the motions of aeroplanes / (London : Macmillan, 1911), by G. H. Bryan (page images at HathiTrust)

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