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Transport planes -- Design and construction -- Mathematical models

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• Transport planes -- Design and construction
• Airplanes -- Design and construction -- Mathematical models
• Mathematical models

• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design (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 P. Aidala, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary (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 Andrew J. Srokowski, P. Aidala, M. E. Lores, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 3 Part 1, User's guide to transport design computer programs (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 R. A. Weed, Andrew J. Srokowski, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design (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 Andrew J. Srokowski, P. R. Simth, R. A. Weed, M. E. Lores, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Lawrence E. Putnam and Langley Research Center (page images at HathiTrust)
• Preliminary analysis of the span-distributed-load concept for cargo aircraft design (National Aeronautics and Space Administration ;, 1975), by Allen H. Whitehead and Langley Research Center (page images at HathiTrust)
• Perspective on the span-distributed-load concept for application to large cargo aircraft design (National Aeronautics and Space Administration ;, 1975), by Allen H. Whitehead and Langley Research Center (page images at HathiTrust)
• Conceptual design study of 1985 commercial VTOL transports that utilize rotors : summary (National Aeronautics and Space Administration ;, 1975), by N. F. K. Kefford, C. L. Munch, Ames Research Center, and United Aircraft Corporation. Sikorsky Aircraft Division (page images at HathiTrust)
• Conceptual design study of improved 1985 remote lift-fan V/Stol commercial transports (National Aeronautics and Space Administration ;, 1975), by Robert L. Cavage, Ames Research Center, and Rockwell International (page images at HathiTrust)
• V/STOL lift fan commercial short-haul transports : continuing conceptual design study (National Aeronautics and Space Administration ;, 1974), by J. M. Zabinsky, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Conceptual engineering design studies of 1985-era commercial VTOL and STOL transports that utilize rotors (National Aeronautics and Space Administration ;, 1975), by J. P. Magee, Colin A. Widdison, R. D. Clark, Ames Research Center, and Boeing Vertol Company (page images at HathiTrust)
• Conceptual design studies of candidate V/STOL lift fan commercial short haul transport for 1980-85 V/STOL lift fan study (National Aeronautics and Space Administration ;, 1973), by William M. Eldridge, Ames Research Center, and Boeing Company (page images at HathiTrust)
• Conceptual design study of a V/STOL lift fan commercial short haul transport (National Aeronautics and Space Administration ;, 1973), by Ronald G. Knight, Jerome A. Prizlow, William V. Powell, Ames Research Center, and North American Rockwell Corporation (page images at HathiTrust)

• Aircraft design for mission performance using nonlinear multiobjective optimization methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division :, 1990), by Augustine R. Dovi, Gregory A. Wrenn, and Langley Research Center (page images at HathiTrust)
• Computer program to perform aircraft design synthesis. Volume II, Technical volume (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by B. H. Oman, T. F. Reed, N. P. Karil, S. K. Pederson, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Convair Division (page images at HathiTrust)

• CTOL transport technology, 1978 : proceedings of a conference held at Langley Research Center, Hampton, Virginia, February 28-March 3, 1978. (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978), by NASA CTOL Transport Technology Conference (1978 : Langley Research Center) and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Military aircraft : C-17 wing flap requires additional testing : report to the Secretary of the Air Force (The Office ;, 1992), by United States General Accounting Office and United States Air Force (page images at HathiTrust)

• Problems of designing passenger aircraft (National Aeronautics and Space Administration, 1975), by V. M. Sheĭnin and V. I. Kozlovskiĭ (page images at HathiTrust)
• Application of active controls technology to the NASA JetStar airplane (National Aeronautics and Space Administration ;, 1975), by R. H. Lange, Flight Research Center (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method (National Aeronautics and Space Administration ;, 1975), by Larry Wayne Mohn, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• High-transonic-speed transport aircraft study : summary report (National Aeronautics and Space Administration ;, 1974), by Robert M. Kulfan, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• The effect of winglets on the static aerodynamic stability characteristics of a representative second generation jet transport model (U.S. National Aeronautics and Space Administration ;, 1976), by Peter F. Jacobs, Stuart G. Flechner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design analysis of wide body aircraft : report (U.S. Govt. Print. Office, 1979), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and Oversight (page images at HathiTrust)
• Drag measurements of upswept afterbodies and analytical study on axisymmetric separation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Mansop Hahn, Theodore C. Nark, Paul E. Rubbert, Gunter W. Brune, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Commercial Airplane Company (page images at HathiTrust)

• Development of Integrated Programs for Aerospace-Vehicle Design (IPAD) : reference design process (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Donald D. Meyer, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)

• Design analysis of wide-body aircraft hearings before the Subcommittee on Investigations and Oversight of the Committee on Science and Technology, U.S. House of Representatives, Ninety-sixth Congress, first session ... (U.S. Govt. Print. Office, 1980), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and Oversight (page images at HathiTrust)

• Aircraft certification : limited progress on developing international design standards (General Accounting Office, 1992), by United States General Accounting Office (page images at HathiTrust)

• Effects of winglets on first-generation jet transport wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Stuart G. Flechner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

• Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model (National Aeronautics and Space Administration ;, 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)
• Concept development of a Mach 4 high-speed civil transport (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Christopher S. Domack and Langley Research Center (page images at HathiTrust)
• Materials for the supersonic transport. (National Aeronautics and Space Administration, 1965), by M. S. Healy, Battelle Memorial Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental study of the validity of the heat-field concept for sonic-boom alleviation (National Aeronautics and Space Administration ;, 1974), by Rudolph J. Swigart, Langley Research Center, and Aerospace Corporation (page images at HathiTrust)
• 1989 high-speed civil transport studies (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Douglas Aircraft Company. HSCT Concept Development Group and Langley Research Center (page images at HathiTrust)
• High-speed civil transport study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Boeing Commercial Airplane Company. New Airplane Development Group and Langley Research Center (page images at HathiTrust)
• Study of high-speed civil transports (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Douglas Aircraft Company. New Commercial Programs and Langley Research Center (page images at HathiTrust)
• Study of high-speed civil transports : summary (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Douglas Aircraft Company. New Commercial Programs and Langley Research Center (page images at HathiTrust)
• An exploratory investigation of a transport configuration designed for supersonic cruise flight near a Mach number of 3 (National Aeronautics and Space Administration, 1960), by Ausley B. Carraway, Melvin M. Carmel, Donald T. Gregory, and Langley Research Center (page images at HathiTrust)
• Application of sonic-boom minimization concepts in supersonic transport design (National Aeronautics and Space Administration ;, 1973), by Harry W. Carlson, Robert J. Mack, Raymond L. Barger, and Langley Research Center (page images at HathiTrust)

• Report of the Panel to Review the V-22 Program : hearing before the Committee on Armed Services, United States Senate, One Hundred Seventh Congress, first session, May 1, 2001. (U.S. G.P.O. :, 2002), by United States Senate Committee on Armed Services and United States. Panel to Review the V-22 Program (page images at HathiTrust)
• Report of the Panel to Review the V-22 Program : hearing before the Committee on Armed Services, United States Senate, One Hundred Seventh Congress, first session, May 1, 2001. (U.S. G.P.O. :, 2002), by United States Senate Committee on Armed Services and United States. Panel to Review the V-22 Program (page images at HathiTrust)

• Analysis and preliminary design of an advanced technology transport flight control system (National Aeronautics and Space Administration ;, 1975), by Ronald Frazzini, Darrel Vaughn, Langley Research Center, and Honeywell Inc. Government and Aeronautical Products Division (page images at HathiTrust)

• NASA TN D-1809 (National Aeronautics and Space Administration, 1963), by Richard J. Re, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

• Automated optimum design of wing structures : deterministic and probabilistic approaches (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by S. S. Rao and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Optimality criterion methods in structural optimization (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by N. S. Khot, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Algorithms for zonal methods and development of three dimensional mesh generation procedures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984, 1984), by Joseph L. Steger, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Stanford University. Department of Aeronautics and Astronautics (page images at HathiTrust)

• Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Harry W. Carlson, Christine M. Darden, and Langley Research Center (page images at HathiTrust)

• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design (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 P. Aidala, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary (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 Andrew J. Srokowski, P. Aidala, M. E. Lores, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 3 Part 1, User's guide to transport design computer programs (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 R. A. Weed, Andrew J. Srokowski, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design (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 Andrew J. Srokowski, P. R. Simth, R. A. Weed, M. E. Lores, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)

• Integrated autopilot/autothrottle for the NASA TSRV B-737 aircraft : design and verification by nonlinear simulation (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by Kevin R. Bruce and Langley Research Center (page images at HathiTrust)

More items available under broader and related terms at left.