02666oam 2200649 450 991070268250332120140922113430.0(CKB)5470000002429361(OCoLC)761221787(EXLCZ)99547000000242936120111115j198001 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierDynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients /Bobby W. SandersWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Office,January 1980.1 online resource (iii, 98 pages) illustrationsNASA technical paper ;1531Title from title screen (viewed Sept. 22, 2014)."January 1980.""Performing organization, Lewis Research Center"--Technical report documentation page.Includes bibliographical references (pages 27-28).AirplanesTurbojet enginesAir intakesAirplanesMotorsValvesAerodynamic stabilitynasatBypassesnasatPropulsion system performancenasatSupersonic inletsnasatTurbojet enginesnasatWind tunnel stability testsnasatAirplanesMotorsValvesfastAirplanesTurbojet enginesAir intakesfastAirplanesTurbojet enginesAir intakes.AirplanesMotorsValves.Aerodynamic stability.Bypasses.Propulsion system performance.Supersonic inlets.Turbojet engines.Wind tunnel stability tests.AirplanesMotorsValves.AirplanesTurbojet enginesAir intakes.Sanders Bobby W.1417227United States.National Aeronautics and Space Administration.Scientific and Technical Information Office,Lewis Research Center,OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910702682503321Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients3524889UNINA