The Online Books Page

Airplanes -- Handling characteristics

See also what's at your library, or elsewhere.

Broader terms:

Narrower terms:

Used for:

Airplanes -- Flying qualities
Flying qualities of airplanes
Handling characteristics of airplanes

Filed under: Airplanes -- Handling characteristics

Weight and balance : an important safety consideration for the general aviation pilot. (NTSB, 1974), by United States. National Transportation Safety Board (page images at HathiTrust)
Safe flying for agricultural aviation. (U.S. Dept. of Transportation, Federal Aviation Administration, 1983), by United States Federal Aviation Administration (page images at HathiTrust)
A qualitative flight test investigation of some handling qualities of liaison type airplanes. (Cornell Aeronautical Laboratory, Inc., 1959), by Donald W. Rhoads (page images at HathiTrust)
Analysis of several handling quality topics pertinent to advanced manned aircraft (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967), by Robert L. Stapleford, J. Alfred Tennant, John J. Best, Dunstan Graham, Irving L. Ashkenas, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
A systems analysis view of longitudinal flying qualities (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1960., 1960), by Duane T. McRuer, C. L. Guerre, Irving L. Ashkenas, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities. Technical report AFFDL-TR-65-39. (1965), by Frederick D. Newell (page images at HathiTrust; US access only)
Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Directorate of Laboratories, Air Force Systems Command, 1967., 1967), by Robert L. Swaim, Alonzo J. Connors, and Air Force Flight Dynamics Laboratory (U.S.) (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)
A Piloted evaluation of an oblique-wing research aircraft motion simulation with decoupling control laws (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Robert W. Kempel and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Comparison of flying qualities derived from in-flight and ground-based simulators for a jet-transport airplane for the approach and landing pilot tasks (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by William D. Grantham and Langley Research Center (page images at HathiTrust)
Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA) (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Jack D. Stephenson, Gordon H. Hardy, and Ames 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)
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), by W. S. Hindson, Robert C. Innis, Gordon H. Hardy, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by H. Paul Stough, James M. Patton, Daniel J. DiCarlo, and Langley Research Center (page images at HathiTrust)
Agricultural airplane mission time structure characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by Joseph W. Jewel, 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)
Subsonic maneuver capability of a supersonic cruise fighter wing concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Gregory D. Riebe, Charles H. Fox, and Langley Research Center (page images at HathiTrust)
Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by H. Paul Stough, Steven M. Sliwa, James M. Patton, 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)
Piloted simulation study of the effects of an automatic trim system on flight characteristics of a light twin-engine airplane with one engine inoperative (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Eric C. Stewart, Kenneth R. Yenni, Philip W. Brown, and Langley Research Center (page images at HathiTrust)
Precision controllability of the F-15 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Thomas R. Sisk, Neil W. Matheny, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Recent progress towards predicting aircraft ground handling performance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Thomas J. Yager, Ellis J. White, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Ground-based and in-flight simulator studies of flight characteristics of a twin-fuselage passenger transport airplane during approach and landing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William D. Grantham and Langley Research Center (page images at HathiTrust)
Flight investigation of the VFR and IFR landing approach characteristics and terminal area airspace requirements for a light STOL airplane (National Aeronautics and Space Administration ;, 1974), by Harold L. Crane, Bruce D. Fisher, Kenneth R. Yenni, and Langley Research Center (page images at HathiTrust)
Analysis of oscillatory motion of a light airplane at high values of lift coefficient (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by James G. Batterson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Determination of stability and control parameters of a light airplane from flight data using two estimation methods (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
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)
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)
Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Long P. Yip and Langley Research Center (page images at HathiTrust)
Validation of a flexible aircraft take-off and landing analysis (FATOLA) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Huey D. Carden, John R. McGehee, 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)
Modal control theory and application to aircraft lateral handling qualities design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by S. Srinathkumar, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Ground-based and in-flight simulator studies of low-speed handling characteristics of two supersonic cruise transport concepts (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by William D. Grantham and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (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)
Dynamics of aircraft antiskid braking systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by John A. Tanner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Willard E. Foss, Langley Research Center, 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)
Turbulence and lateral-directional flying qualities (For sale by the National Technical Information Service, 1971), by James A. Franklin, United States National Aeronautics and Space Administration, and Princeton University (page images at HathiTrust)
Turbulence and longitudinal flying qualities (For sale by the National Technical Information Service, 1971), by James A. Franklin, United States National Aeronautics and Space Administration, and Princeton University (page images at HathiTrust)
NASA CR-1789 (National Aeronautics and Space Administration ;, 1972), by B. J. Kuchta, George R. Friedman, United States National Aeronautics and Space Administration, Langley Research Center, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
A study to determine the flight characteristics and handling qualities of variable geometry spacecraft. Volume III, Low L/D concept with fold-down wings (National Aeronautics and Space Administration ;, 1972), by George R. Friedman, B. J. Kuchta, Langley Research Center, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
Satisfactory lateral-directional handling qualities in the landing approach (NASA, 1965), by Robert L. Stapleford, inc Systems Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Flight test data for a Cessna Cardinal (National Aeronautics and Space Administration ;, 1974), by David L. Kohlman, Langley Research Center, and University of Kansas. Center for Research (page images at HathiTrust)
Aircraft motion and passenger comfort data from scheduled commercial airline flights (U.S. National Aeronautics and Space Administration ;, 1976), by Marta G. Gruesbeck, Daniel J. Sullivan, University of Virginia. Dept. of Engineering Science and Systems, and United States National Aeronautics and Space Administration (page images at HathiTrust)
An in-flight simulation of lateral control nonlinearities (National Aeronautics and Space Administration ;, 1975), by David R. Ellis, Narayan W. Tilak, Langley Research Center, and Princeton University. Flight Research Laboratory (page images at HathiTrust)
The landing flare : an analysis and flight-test investigation (National Aeronautics and Space Administration ;, 1975), by Edward Seckel, Langley Research Center, and Princeton University. Flight Research Laboratory (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)
Theoretical frequency response functions and power spectra of the XB-70 response to atmospheric turbulence (National Aeronautics and Space Administration, 1970), by Thomas E. Stenton, United States National Aeronautics and Space Administration, Langley Research Center, and North American Rockwell Corporation (page images at HathiTrust)
XB-70 structural mode control system design and performance analyses (National Aeronautics and Space Administration, 1970), by John H. Wykes, Alva S. Mori, Louis U. Nardi, United States National Aeronautics and Space Administration, Flight Research Center (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
A method for predicting full scale buffet response with rigid wind tunnel model fluctuating pressure data (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Atlee M. Cunningham, and General Dynamics 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)
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)
Analytical and simulator study of advanced transport handling qualities (National Aeronauticas and Space Administration, Scientific and Technical Information Office ;, 1982), by William H. Levison, William W. Rickard, Beranek Bolt, Douglas Aircraft Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David G. Mitchell, David H. Klyde, Bimal L. Aponso, Dryden Flight Research Facility, Inc PRC, and inc Systems Technology (page images at HathiTrust)
Optimal cooperative control synthesis of active displays (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), by Sanjay Gary, D. K. Schmidt, and Dryden Flight Research Facility (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 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)
Summary and analysis of horizontal-tail contribution to longitudinal stability of swept-wing airplanes at low speeds (U.S. G.P.O.], 1959), by Robert H. Neely (page images at HathiTrust)
An evaluation of the handling qualities of seven general aviation aircraft (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1966), by Marvin R. Barber (page images at HathiTrust)
Flight tests under IFR with an STOL transport aircraft (National Aeronautics and Space Administration ;, 1968), by Robert C. Innis, Richard P. Gallant, Curt A. Holzhauser, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Flight comparison of several techniques for determining the minimum flying speed for a large subsonic jet transport (National Aeronautics and Space Administration, 1970), by David A. Kier, United States National Aeronautics and Space Administration, and NASA Dryden Flight Research Center (page images at HathiTrust)
An analytical study of aircraft lateral-directional handling qualities using pilot models (National Aeronautics and Space Administration ;, 1976), by James J. Adams, Frederick L. Moore, and Langley Research Center (page images at HathiTrust)
Flight-path and airspeed control during landing approach for powered-lift aircraft (National Aeronautics and Space Administration ;, 1974), by James A. Franklin, Robert C. Innis, and Ames Research Center (page images at HathiTrust)
Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee (National Aeronautics and Space Administration ;, 1977), by William C. Sleeman, Langley Research Center, United States National Aeronautics and Space Administration, and David R Forsyth (page images at HathiTrust)
Evaluation of the effect of a yaw-rate damper on the flying qualities of a light twin-engine airplane (National Aeronautics and Space Administration :, 1970), by Calvin R. Jarvis, Einar K. Enevoldson, Paul C. Loschke, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)
NASA TN D-5358 (National Aeronautics and Space Administration ;, 1969), by Lawrence W. Taylor, Kenneth W. Iliff, Flight Research Center (U.S.), 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)
Study of the optimum values of several parameters affecting longitudinal handling qualities of VTOL aircraft (National Aeronautics and Space Administration, 1968), by James R. Kelly, John F. Garren, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-4237 (National Aeronautics and Space Administration ;, 1967), by Kenneth W. Goodson and United States National Aeronautics and Space Administration (page images at HathiTrust)
An analysis of the limit-cycle and structural-resonance characteristics of the X-15 stability augmentation system (National Aeronautics and Space Administration, 1967), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
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)
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)
Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study (National Aeronautics and Space Administration ;, 1972), by Robert W. Rainey and Langley Research Center (page images at HathiTrust)
NASA TN D-5466 (National Aeronautics and Space Administration :, 1970), by William D. Grantham, James M. Patton, Perry L. Deal, Frederikc L. Moore, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-6431 (National Aeronautics and Space Administration ;, 1971), by Kenneth J. Szalai, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)
Flight investigation of performance characteristics during landing approach of a large powered-lift jet transport (National Aeronautics and Space Administration, 1967), by Albert W. Hall, Perry L. Deal, Kalman J. Grunwald, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A piloted fixed-base simulator study of low-speed flight characteristics of an arrow-wing supersonic transport design (National Aeronautics and Space Administration ;, 1968), by William D. Grantham, Perry L. Deal, and Langley Research Center (page images at HathiTrust)
Flight-determined stability and control characteristics of the M2-F3 lifting body vehicle (National Aeronautics and Space Administration ;, 1973), by Alex G. Sim and Flight Research Center (U.S.) (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)
Takeoff certification considerations for large subsonic and supersonic transport airplanes using the Ames Flight Simulator for Advanced Aircraft (National Aeronautics and Space Administration ;, 1973), by C. Thomas Snyder, United States Federal Aviation Administration, and Ames Research Center (page images at HathiTrust)
Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap (National Aeronautics and Space Administration ;, 1974), by Lysle P. Parlett, Arthur E. Phelps, Sandy J. Emerling, and Langley Research Center (page images at HathiTrust)
Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 (National Aeronautics and Space Administration, 1974), by Robert W. Kempel, John A. Manke, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Comparisons of in-flight F-111A inlet performance for on- and off-scheduled inlet geometry at Mach numbers of 0.68 to 2.18 (National Aeronautics and Space Administration, 1971), by Richard A. Martin, Donald L. Hughes, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)
The effects of an autopilot on airplane responses to turbulence with emphasis on tail loads (National Aeronautics and Space Administration ;, 1973), by Boyd Perry, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Flight investigation of steep instrument approach capabilities of a T-33 airplane under manual control (National Aeronautics and Space Administration ;, 1965), by Albert W. Hall, Donald J. McGinley, and Langley Research Center (page images at HathiTrust)
Gain selection method and model for coupled propulsion and airframe systems (National Aeronautics and Space Administration, Scientific and Technical Branch ;, 1982), by Patrick C. Murphy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane (National Advisory Committee for Aeronautics, 1951), by James B. Whitten, Donald E. Hewes, Paul A. Hunter, John P. Campbell, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane (National Advisory Committee for Aeronautics, 1951), by B. Porter Brown, James B. Whitten, Robert G. Chilton, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives (National Advisory Committee for Aeronautics, 1952), by Robert O. Schade, James L. Hassell, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane (National Aeronautics and Space Administration, 1960), by United States National Aeronautics and Space Administration and Flight Research Center (U.S.) (page images at HathiTrust)
Conference on Aircraft Operating Problems ; [papers] (Scientific and Technical Information Division, National Aeronautics and Space Administration ; [for sale by the Superintendent of Documents, U.S.Govt.Print.Off.], 1965), by Conference on Aircraft Operating Problems (1965 : Langley Research Center) and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (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, 1944), by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
A study of lightplane stall avoidance and suppression (Dept. of Transportation, Federal Aviation Administration, System Research & Development Service ;, 1977), by David R. Ellis, Princeton University. Flight Research Laboratory, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
Additional flight evaluations of various longitudinal handling qualities in a variable-stability jet fighter (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Charles R. Chalk, United States. Air Force. Air Research and Development Command, and Wright Air Development Center Center (page images at HathiTrust)
Additional flight evaluations of various longitudinal handling qualities in a variable-stability jet fighter (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Charles R. Chalk, United States. Air Force. Air Research and Development Command, and Wright Air Development Center Center (page images at HathiTrust)
Aeroelastic stability and performance characteristics of aircraft with advanced composite sweptforward wing structures (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), by Terry A. Weisshaar, Air Force Flight Dynamics Laboratory (U.S.), and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Department (page images at HathiTrust)
Analysis of digital flight control systems with flying qualities applications. Volume I, Executive summary (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), by Richard F. Whitbeck, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
An analytical study of V/STOL handling qualities in hover and transition (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 Robert L. Stapleford, Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Theoretical and experimental investigation of some new longitudinal handling qualities parameters (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Henry R. Jex, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
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)
Estimation of flying qualities of piloted airplanes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems command, 1966., 1966), by Robert J. Woodcock, D. E. Drake, Wright-Patterson Air Force Base (Ohio), Douglas Aircraft Company, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Lateral-directional oscillatory 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 I. L. Ashkenas, Wright-Patterson Air Force Base (Ohio), Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Airplane flying characteristics in turbulence (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by E. D. Onstott, E. P. Salmon, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
A flight investigation of lateral-directional handling qualities for V/STOL aircraft in low speed maneuvering flight (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by K. H. Doetsch, D. M. McGregor, D. G. Gould, Air Force Flight Dynamics Laboratory (U.S.), and National Aeronautical Establishment (Canada) (page images at HathiTrust)
Roll 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 I. L. Ashkenas, Wright-Patterson Air Force Base (Ohio), Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Investigation of high-AOA flying qualities : criteria and design guides (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by Donald D. Johnston, Robert K. Heffley, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
Tentative STOL flying qualities criteria for MIL standard and handbook (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Roger H. Hoh, David G. Mitchell, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
Aircraft maneuvers for the evaluation of flying qualities and agility. Volume 2, Maneuver descriptions and section guide (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1993., 1993), by David J. Wilson, Kevin D. Citurs, David R. Riley, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
Aircraft maneuvers for the evaluation of flying qualities and agility. Volume 1, Maneuver development process and initial maneuver set (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1993., 1993), by David J. Wilson, Kevin D. Citurs, David R. Riley, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
Influence of pitching moment characteristics on departure and uncoordinated roll reversal boundaries for fighter configurations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force WRight Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by William. Jr Bihrle, B. Barnhart, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Inc Bihrle Applied Research (page images at HathiTrust)
Human pilot dynamics in compensatory systems: theory, models and experiments with controlled element and forcing function variations (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Frorce Systems Command, 1965), by inc Systems Technology, Duane T. McRuer, and Pa.). Laboratories for Research and Development Franklin Institute (Philadelphia (page images at HathiTrust)

More items available under narrower terms.

Help with reading books -- Report a bad link -- Suggest a new listing

Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials

Books -- News -- Features -- Archives -- The Inside Story

Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.