01996oam 2200565 450 991070618910332120170818150632.0(CKB)5470000002454532(OCoLC)703664188(EXLCZ)99547000000245453220110224j199902 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFactors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /W.G. Steenken [and three others]Edwards, California :National Aeronautics and Space Administration, Dryden Flight Research CenterFebruary 1999.1 online resource (vii, 191 pages) illustrationsNASA/TM ;1999-206572"February 1999.""Performing organization: NASA Dryden Flight Research Center"--Report documentation page.Includes bibliographical references (page 34).F-18 aircraftnasatAerodynamic stabilitynasatAngle of attacknasatCompressorsnasatControl surfacesnasatFlight controlnasatResearch vehiclesnasatRotorsnasatSubsonic speednasatF-18 aircraft.Aerodynamic stability.Angle of attack.Compressors.Control surfaces.Flight control.Research vehicles.Rotors.Subsonic speed.Steenken William G.1392405Dryden Flight Research Facility,SSNSSNGPOBOOK9910706189103321Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F3502513UNINA