The Online Books Page

Airplanes -- Flight testing

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

• Airplanes
• Flight testing
• Airplanes -- Testing

• Airplanes -- Flight testing -- 20th century
• Airplanes -- Flight testing -- Bibliography
• Airplanes -- Flight testing -- Computer programs
• Airplanes -- Flight testing -- Congresses
• Airplanes -- Flight testing -- Data processing
• Airplanes -- Flight testing -- International cooperation
• Airplanes -- Flight testing -- Mathematical models
• Airplanes -- Turbojet engines -- In-flight monitoring
• Airplanes, Military -- Flight testing
• Jet planes -- Flight testing
• Supersonic planes -- Flight testing
• Airplanes -- California -- Flight testing
• Airplanes -- Ohio -- Dayton -- Flight testing
• Airplanes -- United States -- Flight testing

• Flight testing of airplanes

• Always another dawn; the story of a rocket test pilot (World Pub. Co., 1960), by A. Scott Crossfield and Clay Blair (page images at HathiTrust)
• Flight test manual. (Pergamon Press, 1959), by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development (page images at HathiTrust)
• Career opportunities. (Air Force Flight Test Center, [1985?], 1985), by Air Force Flight Test Center (U.S.) (page images at HathiTrust)
• Flight research : problems encountered and what they should teach us (NASA History Division, Office of Policy and Plans, NASA Headquarters, 2000), by Milton O. Thompson, J. D. Hunley, and United States. National Aeronautics and Space Administration. History Office (page images at HathiTrust)
• AIA test flying operations, continental U.S., 1958. (Buffalo, 1960), by Cornell Aeronautical Laboratory (page images at HathiTrust)
• Simulation of the effects of winds and turbulence upon longitudinal motions of an aircraft flying at low altitude and high speed. (Cornell Aeronautical Laboratory, inc. Flight Research Dept., 1960), by Charles Boris Notess (page images at HathiTrust)
• Proposed ground and flight check-out of variable L/D system installed in variable stability T-33 (Cornell Aeronautical Laboratory, inc., Buffalo, 1961), by Cornell Aeronautical Laboratory. Flight Research Department and Charles Chalk (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)
• Flight evaluations of the effect of variable spiral damping in a JTB-26B airplane. (Cornell Aeronautical Laboratory, Inc., 1957), by Donald W. Rhoads (page images at HathiTrust)
• Investigation of a technique for improving aircraft response using a complementary optimum-response model. (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1958), by Raymond R. Rath (page images at HathiTrust)
• Effect of motion cues during complex curved approach and landing tasks : a piloted simulation study (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Charles Scanlon and Langley Research Center (page images at HathiTrust)
• Flight control systems development and flight test experience with the HiMAT research vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Robert W. Kempel, Michael R. Earls, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Flight testing of aircraft (National Aeronautics and Space Administration ;, 1967), by M. G. Kotik (page images at HathiTrust)
• Experiments in sensing transient rotational accelaration cues on a flight simulator (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Russell V. Parrish, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Application of modified profile analysis to function testing of the motion/no-motion issue in an aircraft ground-handling simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Russell V. Parrish, George G. Steinmetz, Burnell T. McKissick, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Application of modified profile analysis to function testing of simulated CTOL transport touchdown-performance data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Russell V. Parrish, Burnell T. McKissick, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Investigation of installation effects on twin-engine convergent-divergent nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by E. Ann Bare, Bobby L. Berrier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experiments in a three-dimensional adaptive-wall wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Edward T. Schairer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Miniature flow-direction and airspeed sensor for airplanes and radio-controlled models in spin studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by David D. Kershner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Light airplane crash tests at three roll angles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Claude B. Castle, Emilio Alfaro-Bou, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight assessment of a large supersonic drone aircraft for research use (National Aeronautics and Space Administration ;, 1975), by Clinton V. Eckstrom, Ellwood L. Peele, and Langley Research Center (page images at HathiTrust)
• Important factors in the maximum likelihood analysis of flight test maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Kenneth W. Iliff, T. D. Montgomery, Richard E. Maine, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Wind-tunnel investigation of the validity of a sonic-boom-minimization concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Robert J. Mack, Christine M. Darden, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Similitude requirements and scaling relationships as applied to model testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Simulator evaluation of separation of display parameters in path-following tasks (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Garimella R. Sarma, James J. Adams, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Parametric study of microwave-powered high-altitude airplane platforms designed for linear flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Charles E. K. Morris, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Application of a performance modeling technique to an airplane with variable sweep wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Paul C. Redin, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• A conceptual framework for using Doppler radar acquired atmospheric data for flight simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Warren Campbell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Comparison of simulator fidelity model predictions with in-simulator evaluation data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Russell V. Parrish, Billy R. Ashworth, Burnell T. McKissick, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight test of a pure-tone acoustic source (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Arnold W. Mueller, John S. Preisser, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude (National Aeronautics and Space Administration Scieentific and Technical Information Branch ;, 1983), by David M. Straight, Richard R. Cullom, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight tests of the Digital Integrated Automatic Landing System (DIALS) (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Nesim Halyo, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Incorporated Information & Control Systems (page images at HathiTrust)
• Flight test results of a trailing edge flap designed for direct-lift control (National Aeronautics and Space Administration ;, 1969), by Charles R. Taylor, Boeing Company, and Ames Research Center (page images at HathiTrust)
• Geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment (National Aeronautics and Space Administration ;, 1971), by Paul M. Kenner, Ralph B. Holt, Frederic T. Churchill, United States National Aeronautics and Space Administration, Langley Research Center, and Vought Missiles and Space Division LTV Aerospace Corporation (page images at HathiTrust)
• The experimental determination of atmospheric absorption from aircraft acoustic flight tests (National Aeronautics and Space Administration :, 1971), by R. L. Miller, P. B. Oncley, United States National Aeronautics and Space Administration, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Investigation of Northrop F-5A wing buffet intensity in transonic flight (National Aeronautics and Space Administration ;, 1974), by Chintsun Hwang, W. S. Pi, Ames Research Center, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Numerical and flight simulator test of the flight deterioration concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by John McCarthy, Vern Norviel, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight evaluation of a spoiler roll control system on a light twin-engine airplane (National Aeronautics and Space Administration ;, 1978), by David L. Kohlman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Closed loop models for analyzing engineering requirements for simulators (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Sheldon Baron, David L. Kleinman, Ramal Muralidharan, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An optimal control model approach to the design of compensators for simulator delay (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Sheldon Baron, Roy Lancraft, A. Caglayan, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Beranek Bolt, and Ames Research Center (page images at HathiTrust)
• NASA TN D-2017 (National Aeronautics and Space Administration, 1963), by James L. Raper, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• NASA TN D-6198 (National Aeronautics and Space Administration ;, 1971), by William A. Newsom, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Flight investigation of the roll requirements for transport airplanes in cruising flight (National Aeronautics and Space Administration ;, 1970), by Euclid C. Holleman, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5491 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by L. Stewart Rolls, Ronald M. Gerdes, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5342 (National Aeronautics and Space Administration :, 1969), by Frank R. Niessen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data (National Aeronautics and Space Administration ;, 1971), by J. W. Usry, John W. Wallace, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static force tests of a model of a twin-jet fighter airplane for angles of attack from -10⁰ to 110⁰ and sideslip angles from -40⁰ to 40⁰ (National Aeronautics and Space Administration, 1971), by Ernie L. Anglin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• General solutions of optimum problems in nonstationary flight (NACA, 1955), by Angelo Miele, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Crash tests of four low-wing twin-engine airplanes with truss-reinforced fuselage structure (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by M. Susan Williams, Edwin L. Fasanella, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Comparison of three thrust calculation methods using in-flight thrust data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Donald L. Hughes, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight techniques for determining airplane drag at high Mach numbers (National Advisory Committee for Aeronautics, 1956), by De E. Beeler, Edwin J. Saltzman, Donald R. Bellman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree swept-back wing. (National Advisory Committee for Aeronautics, 1955), by Richard S. Bray, Robert C. Innis, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds (National Advisory Committee for Aeronautics, 1957), by Gareth H. Jordan, Stanley P. Butchart, Earl R. Keener, Flight Research Center (U.S.), United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of a 90° cross wind on the take-off distance of a light airplane equipped with a cross-wind landing gear (National Advisory Committee for Aeronautics, 1949), by Seth B. Anderson, William H. McAvoy, Burnett L. Gadeberg, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane (National Advisory Committee for Aeronautics, 1949), by Charles J. Liddell, Donovan R. Heinle, Rudolph D. Van Dyke, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A flight investigation of the effects of compressibility on applied gust loads (National Advisory Committee for Aeronautics, 1949), by E. T. Binckley, Jack Funk, 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)
• Calibration of strain-gage installations in aircraft structures for the measurement of flight loads (National Advisory Committee for Aeronautics, 1953), by T. H. Skopinski, Wilber B. Huston, William S. Aiken, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Full flight performance testing. (Airplane Engineering Dept., 1918) (page images at HathiTrust)
• Controllability of the X-15 research airplane with interim engines during high-altitude flights (National Aeronautics and Space Administration, 1961), by Euclid C. Holleman, Donald Reisert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight investigation at supersonic speeds of the stability and drag of a 79° clipped delta boost-glide configuration including an analog study of coupled motions during the flight (National Aeronautics and Space Administration, 1961), by Sherwood Hoffman, Willard S. Blanchard, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flight and analytical study of roll requirements of a fighter airplane (National Advisory Committee for Aeronautics, 1956), by James J. Adams and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analytical determination of flight characteristics of aircraft (Sandia Corporation ;, 1959), by Alphonse Iacoletti and Sandia Corporation (page images at HathiTrust; US access only)
• Flight tests of experimental beveled-trailing-edge Frise ailerons on a fighter airplane (National Advisory Committee for Aeronautics ;, 1946), by R. Fabian Goranson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• High-altitude flight cooling investigation of a radial air-cooled engine (National Advisory Committee for Aeronautics ;, 1946), by Eugene J. Manganiello, E. Barton Bell, Michael F. Valerino, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight measurements of the flying qualities of five light airplanes (National Advisory Committee for Aeronautics, 1948), by Paul A. Hunter and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1941), by Lewis A. Rodert, Lawrence A. Clousing, William H. McAvoy, Ames Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1945), by William N. Turner, Lawrence A. Clousing, Paul J. Steffen, 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)
• Lift-curve slopes determined in flight on a flexible swept-wing jet bomber (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), by William S. Aiken, Raymond A. Fisher, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight tests of the United Air Lines stall warning system (Washington : U.S. Dept. of Commerce, Civil Aeronautics Administration, 1945., 1945), by C. J. Janes and United States. Civil Aeronautics Administration (page images at HathiTrust)
• Investigations of vertical displays of altitude information : I. comparison of a moving-tape and standard altimeter on a simulated flight task (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1958., 1958), by Robert F. Mengelkoch, Robert C. Houston, United States. Air Force. Air Research and Development Command, University of Illinois, and Wright Air Development Center (page images at HathiTrust)
• Investigations of vertical displays of altitude information : II. the effect of practice on performance of a simulated flight task using a moving-tape altimeter (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1958., 1958), by Robert F. Mengelkoch, Robert C. Houston, United States. Air Force. Air Research and Development Command, University of Illinois, and Wright Air Development Center (page images at HathiTrust)
• On pulse shapes suitable for flight tests (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research Development and Command, United States Air Force, 1958., 1958), by Furman. Jr Stout, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• An analytical study of the dynamics of spinning aircraft. Part I. Flight test data analyses and spin calculations (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by John H. Wykes, Richard A. Collins, Gilbert R. Casteel, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and North American Aviation (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)
• Prediction of six-degree-of-freedom store separation trajectories at speeds up to the critical speed. Volume I, Theoretical methods and comparisons with experiment (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1974, 1974), by Frederick K. Goodwin, Jack Norman Nielsen, Marnix F. E. Dillenius, Air Force Flight Dynamics Laboratory (U.S.), Nielsen Engineering & Research, and United States. Air Force. Systems Command (page images at HathiTrust)
• Flexible-wing manned test vehicle (Fort Eustis, Virginia : U.S. Army Transportation Research Command, 1962., 1962), by Ryan Aeronautical Company and United States. Army. Transportation Research Command (page images at HathiTrust)
• The determination of aircraft stability coefficients from flight test data : Part 1 : Theoretical considerations (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by L. E. Wilkie, Luciano L. Mazzola, Meredith N. Springer, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Massachusetts Institute of Technology. Aeronautical Engineering Department (page images at HathiTrust)
• The determination of aircraft stability coefficients from flight-test data : Part 2 : Longitudinal investigations (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by L. E. Wilkie, Meredith N. Springer, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Massachusetts Institute of Technology. Aeronautical Engineering Department (page images at HathiTrust)

More items available under narrower terms.