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Online Books by

Douglas Aircraft Company

Books from the extended shelves:

• Douglas Aircraft Company: 50th anniversary of naval aviation, 1911-1961 (El Segundo, Calif., 1962), also by Bob Meakin (page images at HathiTrust)
• Douglas Aircraft Company: Aircraft alerting systems standardization study, phase I : final report (Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service ;, 1980), also by G. P. Boucek, Lockheed Aircraft Corporation, Boeing Company, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
• Douglas Aircraft Company: Analytical and simulator study of advanced transport handling qualities (National Aeronauticas and Space Administration, Scientific and Technical Information Office ;, 1982), also by William H. Levison, William W. Rickard, Beranek Bolt, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Douglas Aircraft Company: B-66B low level gust study. Volume XI, Crew Comments. Part 2, Flights G-54-G115 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Dynamics Laboratory, Air Research and Development Command, United States Air Force, 1961., 1961), also by Air Force Flight Dynamics Laboratory (U.S.), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Douglas Aircraft Company: Biaxial fracture strength of brittle materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Henry W. Babel, Air Force Materials Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Douglas Aircraft Company: Development of an empirically based computer program to predict the aerodynamic characteristics of aircraft. Volume I, Basic Theoretical methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by M. L. Goldhammer, C. C. Shen, M. L. Lopez, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: Discontinuity stresses in shells general model (Missile & Space Systems Division, Douglas Aircraft Co., 1962), also by R. R. Meyer (page images at HathiTrust)
• Douglas Aircraft Company: Effect of compressive loads on structural fatigue at elevated temperature (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Douglas Aircraft Company: Electron fractography handbook (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by A. Phillips, B. V. Whiteson, V. Kerlins, Air Force Materials Laboratory (U.S.), and United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
• Douglas Aircraft Company: 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), also by Robert J. Woodcock, D. E. Drake, Wright-Patterson Air Force Base (Ohio), and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: An Exploration of function analysis and function allocation in the commercial flight domain (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by James C. McGuire and Langley Research Center (page images at HathiTrust)
• Douglas Aircraft Company: Flat plates under normal loads. (Santa Monica, 1937) (page images at HathiTrust)
• Douglas Aircraft Company: Flight phase status monitor study : phase I, systems concepts (Federal Aviation Administration, Program Engineering and Maintenance Service ;, 1984), also by L. G. Summers, Lockheed Aircraft Corporation, Boeing Commercial Airplane Company, and United States. Federal Aviation Administration. Program Engineering & Maintenance Service (page images at HathiTrust)
• Douglas Aircraft Company: Flight propulsion control coupling for thrust vectoring fighter aircraft. Volume III, Phase II (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980., 1980), also by Frederick C. Glaser and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: FORMAT : Fortran matrix abstraction technique. Volume 5, Supplement II. Engineering user and technical report-extended (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), also by John Pickard, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Douglas Aircraft Company: Handbook of the physical properties of the planet Venus (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1967), also by Lloyd Randall Koenig (page images at HathiTrust)
• Douglas Aircraft Company: Influence of environment on ceramic properties (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), also by George R. Pulliam, Bruce G. Leonard, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Douglas Aircraft Company: Instability of laminar separation bubbles : causes and effects (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1987., 1987), also by Tuncer Cebeci and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Douglas Aircraft Company: Interactive composite joint design. Part 1, Final technical report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. K. Smith, C. G. Dietz, L. J. Hart-Smith, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: Interactive composite joint design. Part 3, Programming manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. K. Smith, C. G. Dietz, L. J. Hart-Smith, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: Investigation into more complete use of structural materials through a study of the stress-temperature-time conditions of a re-entry vehicle (Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1961), also by J. E. Davis (page images at HathiTrust)
• Douglas Aircraft Company: Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communities (National Aeronautics and Space Administration ;, 1970), also by Langley Research Center (page images at HathiTrust)
• Douglas Aircraft Company: Investigation of thermal effects on structural fatigue (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), also by United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and Douglas Aircraft Company. Santa Monica Division (page images at HathiTrust)
• Douglas Aircraft Company: Lunar orbit mission analysis for the improved delta launch venicle and AIMP-D spacecraft (National Aeronautics and Space Administration ;, 1967), also by D. L. Mootchnik, J. Kork, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• Douglas Aircraft Company: The Mark IV Supersonic-Hypersonic Arbitrary-body Program. Volume I, User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Arvel E. Gentry, Wayne R. Oliver, Douglas N. Smyth, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: The Mark IV Supersonic-Hypersonic Arbitrary-body Program. Volume II, Program formulation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Arvel E. Gentry, Wayne R. Oliver, Douglas N. Smyth, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: Methods for predicting the aerodynamic and stability and control characteristics of STOL aircraft. Volume II, STOL aerodynamic methods computer program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by M. I. Goldhammer, N. F. Wasson, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: Methods for predicting the aerodynamic and stability and control characteristics of STOL aircraft. Volume III, Engineering methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by M. I. Goldhammer, M. L. Lopez, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: Noise and sonic fatigue of high lift devices. aeroacoustic loads (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by H. L. Leve, D. A. Plocher, C. M. Ho, M. A. Yeneriz, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and University of Southern California (page images at HathiTrust)
• Douglas Aircraft Company: Parametric study of STOL short-haul transport engine cycles and operational techniques to minimize community noise impact (National Aeronautics and Space Administration, 1974), also by Ames Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Douglas Aircraft Company: Reduction of drag due to lift at supersonic speeds (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1955), also by E. W. Graham (page images at HathiTrust)
• Douglas Aircraft Company: Report of an engineering leadership training course ([Scacramento], 1945), also by California. Bureau of Industrial Education (page images at HathiTrust)
• Douglas Aircraft Company: Service evaluation of airborne tire pressure indicating systems (Federal Aviation Administration, Systems Research & Development Service ;, 1982), also by W. Kwong, Federal Aviation Administration Technical Center (U.S.), and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
• Douglas Aircraft Company: Shock and vibration flight data ... (National Aeronautics and Space Administration, 1965), also by E. C. Meltzer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Douglas Aircraft Company: Solar eclipse flight expedition (Douglas Aircraft Co., 1963), also by Wolfgang B. Klemperer and National Geographic Society (U.S.) (page images at HathiTrust)
• Douglas Aircraft Company: The solution of laminar boundary layer equations by the finite differnce method (Santa Monica, Cal., 1960), also by J. C. Wu (page images at HathiTrust)
• Douglas Aircraft Company: Some considerations in the fatigue design of launch and spacecraft structures (National Aeronautics and Space Administration ;, 1965), also by R. H. Christensen and R. J. Bellinfante (page images at HathiTrust)
• Douglas Aircraft Company: Some problems of the calculation of three-dimensional boundary-layer flows on general configurations (National Aeronautics and Space Administration ;, 1973), also by Tuncer Cebeci and Langley Research Center (page images at HathiTrust)
• Douglas Aircraft Company: Theoretical analysis of light plane landing and take-off accidents due to encountering the wakes of large airplanes (Douglas Aircraft Company, 1954), also by Zegmund O. Bleviss (page images at HathiTrust)
• Douglas Aircraft Company: Trim drag at supersonic speeds of various delta-planform configurations (National Aeronautics and Space Administration, 1960), also by M. E. Graham and B. M. Ryan (page images at HathiTrust)
• Douglas Aircraft Company: USAF stability and control datcom (National Technical Information Service, 1975), also by R. D. Finck and D. E. Hoak (page images at HathiTrust)
• Douglas Aircraft Company: VISCID/INVISCID separated flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by Tuncer Cebeci, S. M. Schimke, D. P. Mack, R. W. Clark, K. C. Chang, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• Douglas Aircraft Company: Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78 (National Aeronautics and Space Administration ;, 1977), also by O. D. Wells and United States National Aeronautics and Space Administration (page images at HathiTrust)

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