Airplanes -- Jet propulsion -- ModelsSee also what's at your library, or elsewhere.
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Filed under: Airplanes -- Jet propulsion -- Models
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Filed under: Airplanes -- Jet propulsion- Aircraft and Missile Propulsion (2 volumes (third apparently never published); New York: J. Wiley and Sons; London: Chapman and Hall, c1958), by Maurice J. Zucrow (page images at HathiTrust)
- High speed aerodynamics and jet propulsion. (Princeton University Press, 1955) (page images at HathiTrust)
- Jet aircraft simplified (Aero Pubs., 1953), by Charles Edward Chapel (page images at HathiTrust)
- Jets, rockets, and guided missiles (McBride, 1951), by David C. Cooke (page images at HathiTrust)
- Gas turbines for aircraft (McGraw-Hill Book Co., 1949), by F. W. Godsey and Lloyd Arthur Young (page images at HathiTrust)
- Random vibration (M.I.T. Press, 1959), by Stephen H. Crandall (page images at HathiTrust)
- Turbine- and jet-propelled aircraft powerplants. (Chartwell House, 1954), by James P. Eames (page images at HathiTrust)
- Studies of noise characteristics of the Boeing 707-120 jet airliner and of large conventional propeller-driven airliners, prepared for the Port of New York Authority. (Cambridge, 1958), by Beranek Bolt and Port of New York Authority (page images at HathiTrust)
- Studies of noise characteristics of the Comet 4 jet airliner and of large conventional propeller-driven airliners, prepared for the Port of New York Authority. (Cambridge, 1958), by Beranek Bolt and Port of New York Authority (page images at HathiTrust)
- Pulse reactor lift-propulsion system development program : final report, Bureau of Naval Weapons, contract no. 61-9226-c (Bureau of Naval Weapons?, 1963), by Raymond Marshall Lockwood (page images at HathiTrust)
- Air pollution created by aircraft jet engine emissions. Joint hearing before the Committee on Commerce and the Subcommittee on Air and Water Pollution of the Committee on Public Works, United States Senate, Ninety-first Congress, second session ... February 4, 1970. (U.S. Govt. Print. Off., 1970), by United States. Congress. Senate. Committee on Commerce. Subcommittee on Surface Transportation and United States. Congress. Senate. Committee on Public Works. Subcommittee on Air and Water Pollution (page images at HathiTrust)
- The finite aspect ratio jet flap. (Cornell Aeronautical Laboratory, 1959), by Richard A. Hartunian (page images at HathiTrust)
- Elements of flight propulsion (Wiley, 1960), by Joseph V Foa (page images at HathiTrust)
- Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Bobby L. Berrier, John G. Taylor, and Langley Research Center (page images at HathiTrust)
- Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Francis J. Capone, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
- Progress in supersonic cruise aircraft technology (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Cornelius Driver and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Jet engine exhaust emissions of high-altitude commercial aircraft projected to 1990 (National Aeronautics and Space Administration, 1974), by Jack Grobman, Robert D. Ingebo, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Aircraft ground tests and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Steven A. Johnson and Dryden Flight Research Facility (page images at HathiTrust)
- Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 (U.S. National Aeronautics and Space Administration ;, 1976), by Francis J. Capone and Langley Research Center (page images at HathiTrust)
- Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction (U.S. National Aeronautics and Space Administration ;, 1976), by Robert J. Shaw, Harvey E. Neumann, Joseph F. Wasserbauer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Venturi nozzle effects on fuel drop size and nitrogen oxide emissions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Susan M. Johnson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
- Ignition of SiH₄-H₂-0₂-N₂ behind reflected shock waves (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Allen G. McLain, R. Clayton Rogers, Casimir J. Jachimowski, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Validation of scramjet exhaust simulation technique (National Aeronautics and Space Administration ;, 1976), by H. B. Hopkins, J. Leng, H. B. Konopka, United States National Aeronautics and Space Administration, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
- 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), by O. D. Wells, Douglas Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Infrared measurements of a scramjet exhaust (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by R. A. Reed, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Control of gas-turbine and ramjet engines (National Aeronautics and Space Administration, 1961), by L. A. Zalmanzon, Boris Aleksandrovich Cherkasov, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- The effects on propulsion-induced aerodynamic forces of vectoring a partial-span rectangular jet at Mach numbers from 0.40 to 1.20 (National Aeronautics and Space Administration ;, 1975), by Francis J. Capone and Langley Research Center (page images at HathiTrust)
- Exploratory study of transient unstart phenomena in a three-dimensional fixed-geometry scramjet engine (U.S. National Aeronautics and Space Administration ;, 1976), by Allan R. Wieting and Langley Research Center (page images at HathiTrust)
- Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane (National Aeronautics and Space Administration ;, 1976), by William J. Small, P. J. Johnston, John P. Weidner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-6679 (National Aeronautics and Space Administration :, 1972), by Donald L. Hughes, Harold J. Johnson, Jon K. Holzman, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Steady-state and dynamic pressure phenomena in the propulsion system of an F-111A airplane (National Aeronautics and Space Administration ;, 1973), by Frank W. Burcham, Jon K. Holzman, Donald L. Hughes, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)
- Aircraft utilization and propulsion reliability report (U.S. Dept. of Transportation, Federal Aviation Administration, Flight Standards National Field Office, in the 20th century), by United States. Flight Standards National Field Office and United States. Aviation Standards National Field Office (page images at HathiTrust)
- Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, Robert O. Jr Dietz, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of turbine performance and effect of tail-pipe design on engine performance (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frederick C. Foshag, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Pressure-sensitive system for gas-temperature control (National Advisory Committee for Aeronautics, 1948), by Norman Matz, Richard S. Cesaro, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Bemrose Boyd, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of turbine performance of 19B-8 engine (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frank L. Suozzi, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Operational characteristics (National Advisory Committee for Aeronautics, 1948), by Richard L. Golladay, Stanley L. Gendler, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Analysis of compressor performance (National Advisory Committee for Aeronautics, 1948), by Robert O. Dietz, John K. Kuenzig, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Operational characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Analysis of combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Reece V. Hensley, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
- Jets (NAEC Materials of Instruction Committee, 1953), by National Aviation Education Council. Materials of Instruction Committee (page images at HathiTrust; US access only)
- Dynamic performance of high bypass ratio turbine engines with water ingestion (National Aeronautics and Space Administration, Lewis Research Center, 1996), by S. N. B. Murthy, Federal Aviation Administration Technical Center (U.S.), Purdue University, and Lewis Research Center (page images at HathiTrust)
- Quantitative determination of engine water ingestion (Federal Aviation Administration Technical Center ;, 1986), by P. Parikh, V. Sarohia, M. Hernan, Jet Propulsion Laboratory (U.S.), and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
- Thrust augmentation study of high performance ejectors (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), by John E. Minardi, Hans von Ohain, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
- Introduction to jet engine fundamentals (The Corporation, 1958), by United Aircraft Corporation / Pratt & Whitney Aircraft Division (page images at HathiTrust; US access only)
- Jet engine mechanic (AFSC 42652) (Extension Course Institute, Air University, 1985), by Ray M. Paddock, David Crawford, Dorothy W. Fuller, Bev Barnes, United States Department of the Air Force, and Air University (U.S.). Extension Course Institute (page images at HathiTrust)
Filed under: Airplanes -- Jet propulsion -- Automatic control- Integrated flight propulsion control research results using the NASA F-15 HIDEC flight research facility (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James F. Stewart and Dryden Flight Research Facility (page images at HathiTrust)
- Flight-determined benefits of integrated flight-propulsion control systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James F. Stewart, Donald H. Gatlin, Frank W. Burcham, and Dryden Flight Research Facility (page images at HathiTrust)
- Propulsion system/flight control integration and optimization : flight evaluation and technology transition (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Frank W. Burcham, Lawrence P. Myers, Glenn B. Gilyard, and Dryden Flight Research Facility (page images at HathiTrust)
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