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Jet transports -- Design and construction

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• Jet transports
• Airplanes -- Design and construction
• Jet planes -- Design and construction
• Transport planes -- Design and construction
• Design and construction

• Jet transports -- Design and construction -- Management
• McDonnell Douglas DC-10 (Jet transport) -- Design and construction
• Jet transports -- United States -- Design and construction

• 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)

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

• Engineering and the Advancement of Human Welfare: 10 Outstanding Achievements, 1964-1989, by National Academy of Engineering (page images with commentary at NAP)
• Turbine transports : proposed CAA policies for airworthiness certification. (Washington : The Administration, 1953., 1953), by United States. Civil Aeronautics Administration (page images at HathiTrust)
• Operating the jet; a symposium presented to the Sub-committee on Aviation of the Committee on Interstate and Foreign Commerce, together with a report of progress and developments on Jet age planning (U. S. Government Printing Office, 1958), by United States Senate Committee on Interstate and Foreign Commerce and United States. Civil Aeronautics Administration. Jet age planning (page images at HathiTrust; US access only)
• Turbine transports; a report by the CAA Turbine-Powered Transport Evaluation Team. (Washington, 1954), by United States. Civil Aeronautics Administration (page images at HathiTrust)
• An inquiry into the relative merits of turbofan and turboprop aircraft as cargo transports. In compliance with Boeing Transport Division letter dated December 18, 1959, ref. 6-1100-62-124 and HAA PR/7-59 dated December 4, 1959. (Sierra Madre, Calif., 1960), by Hackney Airlift Associates (page images at HathiTrust)
• C-5A and Air Force defense profits policy : hearings before the Subcommittee on International Trade, Finance, and Security Economics of the Joint Economic Committee, Congress of the United States, Ninety-eighth Congress, first session, November 1 and 10, 1983. (U.S. G.P.O., 1985), by Finance United States. Congress. Joint Economic Committee. Subcommittee on International Trade (page images at HathiTrust)
• The Air Force can reduce its stated requirements for strategic airlift crews : report (U.S. General Accounting Office], 1979), by United States General Accounting Office (page images at HathiTrust)
• Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing (National Aeronautics and Space Administration, Scientific and Technical Information Association ;, 1978), by Lawrence C. Montoya, Peter F. Jacobs, Stuart G. Flechner, Hugh L. Dryden Flight Research Center, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A Simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Glenn B. Gilyard and Dryden Flight Research Facility (page images at HathiTrust)
• Experimental results of winglets on first, second, and third generation jet transports (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Stuart G. Fletcher, Peter F. Jacobs, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Edwin E. Lee, Odis C. Pendergraft, and Langley Research Center (page images at HathiTrust)
• Advanced secondary power system for transport aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Anthony C. Hoffman and Lewis Research Center (page images at HathiTrust)
• Advanced control technology and its potential for future transport aircraft (U.S. National Aeronautics and Space Administration ;, 1976), by Hugh L. Dryden Flight Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed aerodynamic characteristics of a transport model having 42.33 ̊swept low wing with supercritical airfoil, double-slotted flaps, and T-tail or low tail (National Aeronautics and Space Administration ;, 1975), by Paul G. Fournier and Langley Research Center (page images at HathiTrust)
• Longitudinal aerodynamic characteristics of a deflected-thrust propulsive-lift transport model (National Aeronautics and Space Administration ;, 1975), by Danny R. Hoad and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Delwin R. Croom, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Vehicle design considerations for active control application to subsonic transport aircraft (National Aeronautics and Space Administration ;, 1974), by L. G. Hofmann, Warren F. Clement, Langley Research Center, McDonnell Douglas Astronautics Company-West, and inc Systems Technology (page images at HathiTrust)
• Investigation of the vibration isolation of commercial jet transport pilots during turbulent air penetration (National Aeronautics and Space Administration, 1970), by Dale W. Schubert, Frank E. Roman, Jerome S. Pepi, United States National Aeronautics and Space Administration, Langley Research Center, and Barry Wright Corporation (page images at HathiTrust)
• NASA TN D-2012 (National Aeronautics and Space Administration, 1963), by William Gracey, Joseph W. Stickle, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Vibrations measured in the passenger cabins of two jet transport aircraft (National Aeronautics and Space Administration ;, 1975), by John J. Catherines, Harland F. Scholl, John S. Mixon, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5129 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Kiyoshi Aoyagi, Paul T. Soderman, Stanley O. Dickinson, Army Aeronautical Research Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Jet-wake effect of a high-bypass engine on wing-nacelle interference drag of a subsonic transport airplane (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by James C. Patterson and Stuart G. Flechner (page images at HathiTrust; US access only)
• Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Lysle P. Parlett, Charles Christian Smith, and Delma C. Freeman (page images at HathiTrust; US access only)
• Behavior of aircraft antiskid braking systems on dry and wet runway surfaces : a velocity-rat-controlled, pressure-bias-modulated system (National Aeronautics and Space Administration ;, 1976), by Sandy M. Stubbs, John A. Tanner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of winglets on a first-generation jet transport wing : I - Longitudinal aerodynamic characteristics of a semispan model at subsonic speeds (National Aeronautics and Space Administration ;, 1977), by Peter F. Jacobs, Lawrence C. Montoya, Stuart G. Flechner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap (National Aeronautics and Space Administration :, 1969), by Lysle P. Parlett, James P. Shivers, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6655 (National Aeronautics and Space Administration :, 1972), by William H. Andrews, Richard R. Larson, Glenn H. Robinson, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Four-engine turbojet transport airplane ... (National Aeronautics and Space Administration, 1970), by Paul A. Hunter, Mary W. Fetner, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Flight investigation of approach and flare from simulated breakout altitude of a subsonic jet transport and comparison with analytical models (National Aeronautics and Space Administration ;, 1974), by Neil W. Matheny and Flight Research Center (U.S.) (page images at HathiTrust)
• NASA TN D-1884 (National Aeronautics and Space Administration, 1963), by Kiyoshi Aoyagi, David H. Hickey, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Dynamic stability derivatives of a jet transport configuration with high thrust-weight ratio and an externally blown jet flap (National Aeronautics and Space Administration ;, 1971), by Sue B. Grafton, Charles C. Smith, Lysle P. Parlett, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A modified Newton-Raphson analysis of flight measurements of the trailing vortices of a heavy jet transport (National Aeronautics and Space Administration ;, 1974), by Lawrence W. Taylor, Milton D. McLaughlin, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of an external-flow jet-flap transport configuration having full-span triple-slotted flaps (National Aeronautics and Space Administration :, 1971), by Lysle P. Parlett, Langley Directorate, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight investigation of the trailing vortices generated by a jumbo jet transport (National Aeronautics and Space Administration ;, 1973), by Harry A. Verstynen, R. Earl Dunham, and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on a medium-range wide-body tri-jet airplane model (National Aeronautics and Space Administration :, 1976), by Delwin R. Croom, Geoffrey M. Williams, Raymond D. Vogler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on an extended-range wide-body tri-jet airplane model (National Aeronautics and Space Administration ;, 1976), by Delwin R. Croom, John A. Thelander, Raymond D. Vogler, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• YC-14 interior noise measurements program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by L. M. Butzel, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Commercial Airplane Company (page images at HathiTrust)
• Transonic scaling effect on a quasi, two-dimensional C-141 airfoil model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by C. F. Lo, W. E. Carleton, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• C-5 Galaxy ([AMC Museum?], 2004), by United States Air Force and United States Department of the Air Force (page images at HathiTrust)

• Flight-determined derivatives and dynamic characteristics of the CV-990 airplane (National Aeronautics and Space Administration ;, 1972), by Glenn B. Gilyard and Flight Research Center (U.S.) (page images at HathiTrust)

• Aviation safety : management improvement needed in FAA's airworthiness directive program : report to the chairman, Subcommittee on Surface Transportation and Subcommittee on Aviation, Committee on Public Works and Transportation, House of Representatives. (U.S. General Accounting Office, 1990), by United States General Accounting Office (page images at HathiTrust)
• Aviation safety : changes needed in FAA's Service Difficulty Reporting Program. (U.S. General Accounting Office, 1991), by Science United States. Congress. Senate. Committee on Commerce and United States General Accounting Office (page images at HathiTrust)

More items available under broader and related terms at left.