Online Books by
McDonnell Douglas Corporation
Books from the extended shelves:
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McDonnell Douglas Corporation: Application of the vortex-lattice method to represent a jet exhausting from a flat plate into a crossflowing stream (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by F. L. Heltsley, R. L. Parker, Martin Marietta Corporation, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)- McDonnell Douglas Corporation: Docket No. 79-2257 (United States : United States Court of Appeals for the Seventh Circuit, 1979., 1979), also by Industrial Indemnity Company and United States Department of Labor (page images at HathiTrust; US access only)
- McDonnell Douglas Corporation: Docket No. 80-1812 (United States : United States Court of Appeals for the Seventh Circuit, 1980., 1980), also by Plesa and American Airlines (page images at HathiTrust; US access only)
- McDonnell Douglas Corporation: Docket No. 84-2774 (United States : United States Court of Appeals for the Seventh Circuit, 1985., 1985), also by Moruzi and Inc American Airlines (page images at HathiTrust; US access only)
- McDonnell Douglas Corporation: Docket No. 85-1224 (United States : United States Court of Appeals for the Seventh Circuit, 1985., 1985), also by Lux (page images at HathiTrust; US access only)
- McDonnell Douglas Corporation: Effect of service environment on F-15 boron/epoxy stabilator (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by T. V. Hinkle, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
- McDonnell Douglas Corporation: Evaluation of the reliability and sensitivity of NDT methods for titanium alloys (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1973., 1973), also by Robert J. Lord, Air Force Materials Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
- McDonnell Douglas Corporation: Evaluation of the reliability and sensitivity of NDT methods for titanium alloys. Volume II (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1974., 1974), also by Robert J. Lord, Air Force Materials Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
- McDonnell Douglas Corporation: Experimental evaluation of inlet drag characteristics in the transonic mach number regime (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by F. D. McVey, E. J. Phillips, J. V. Rejeske, United States. Air Force. Systems Command, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
- McDonnell Douglas Corporation: Experimental evaluation of inlet drag characteristics in the transonic mach number regime (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by F. D. McVey, E. J. Phillips, J. V. Rejeske, United States. Air Force. Systems Command, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
- McDonnell Douglas Corporation: F-4 Service Life Tracking Program (Crack Growth Gages) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Charles R. Saff, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
- McDonnell Douglas Corporation: Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1979), also by D. Brooke, D. V. Vondrasek, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- McDonnell Douglas Corporation: A fuselage/tank structure study for actively cooled hypersonic cruise vehicles--summary (U.S. National Aeronautics and Space Administration ;, 1976), also by C. J. Pirrello, J. E. Stone, A. H. Baker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- McDonnell Douglas Corporation: A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings (National Aeronautics and Space Administration ;, 1977), also by Tuncer Cebeci, Judy A. Ramsey, Kalle Kaups, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- McDonnell Douglas Corporation: Heat-transfer and flow-field tests of the McDonnell Douglas-Martin Marietta space shuttle configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by R. K. Matthews, R. H. Eaves, W. R. Martindale, Martin Marietta Corporation, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
- McDonnell Douglas Corporation: High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by L. C. Koch, L. L. Pagel, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- McDonnell Douglas Corporation: Hydrodynamic studies for electrodialysis (U.S. Dept. of the Interior, 1969), also by Georges Belfort, Gerald A. Guter, and United States. Office of Saline Water (page images at HathiTrust)
- McDonnell Douglas Corporation: Hypersonic airframe structures technology needs and flight test requirements (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by J. E. Stone, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and L. C. Koch (page images at HathiTrust)
- McDonnell Douglas Corporation: Investigation of compatibility barriers between plutonia-238 and noble metals at 1500©�C (Richland, Washington : Donald W. Douglas Laboratories, McDonnell Douglas Astronautics Company, 1973., 1973), also by J. D. Watrous, W. E. Ferguson, J. C. Walker, and U.S. Atomic Energy Commission (page images at HathiTrust)
- McDonnell Douglas Corporation: Low-speed test of translating lip axisymmetric inlets for subsonic transports (National Aeronautics and Space Administration ;, 1974), also by P. A. Henne and Ames Research Center (page images at HathiTrust)
- McDonnell Douglas Corporation: Plutonia/Curia compatibility testing : quarterly report for... (Washington, D.C : United States. Dept. of Energy, 19--, in the 20th century), also by United States. Department of Energy. Office of Scientific and Technical Information, U.S. Atomic Energy Commission. Division of Technical Information, and United States. Department of Energy (page images at HathiTrust)
- McDonnell Douglas Corporation: Requirements study for a biotechnology laboratory for manned earth orbiting missions (National Aeronautics and Space Administration ;, 1969), also by L. T. Kail and United States National Aeronautics and Space Administration (page images at HathiTrust)
- McDonnell Douglas Corporation: Research on porous glass membranes for reverse osmosis (U.S. Dept. of the Interior, Office of Saline Water, 1968), also by F. E. Littman, Gerald A. Guter, and United States. Office of Saline Water (page images at HathiTrust)
- McDonnell Douglas Corporation: Stress corrosion cracking of titanium alloys at ambient temperature in aqueous solutions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1969), also by T. L. Mackay and United States National Aeronautics and Space Administration (page images at HathiTrust)
- McDonnell Douglas Corporation: Study of a fail-safe abort system for an actively cooled hypersonic aircraft : volume I--technical summary (U.S. National Aeronautics and Space Administration ;, 1976), also by C. J. Pirrello, R. L. Herring, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- McDonnell Douglas Corporation: A study of the role of pyrotechnic systems on the space shuttle program (National Aeronautics and Space Administration ;, 1973), also by E. Raymond Lake, V. W. Drexelius, S. J. Thompson, and Langley Research Center (page images at HathiTrust)
- McDonnell Douglas Corporation: Summary of landing gear initial flaws (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 W. T. Fujimoto, J. P. Gallagher, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- McDonnell Douglas Corporation: A theoretical method for the analysis and design of axisymmetric bodies (National Aeronautics and Space Administration ;, 1975), also by T. D. Beatty and Langley Research Center (page images at HathiTrust)
- McDonnell Douglas Corporation: Thermal design for areas of interference heating on actively cooled hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Office ;, 1978), also by R. L. Herring, J. E. Stone, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- McDonnell Douglas Corporation: Wing analysis using a transonic potential flow computational method (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by P. A. Henne, R. M. Hicks, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
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