02491oam 2200661 450 991070788690332120231109022632.0(CKB)5470000002467686(OCoLC)55500054(EXLCZ)99547000000246768620040527j200007 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierStatic performance of six innovative thrust reverser concepts for subsonic transport applications summary of the NASA Langley Innovative Thrust Reverser Test Program /Scott C. Asbury and Jeffrey A. YetterHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,July 2000.1 online resource (30 pages, 334 unnumbered pages) color illustrationsNASA/TM ;2000-210300"July 2000.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 30).Static performance of six innovative thrust reverser concepts for subsonic transport applicationsAirplanesBrakesfastAirplanesDesign and constructionfastAirplanesMotorsThrustfastAirplanesTurbofan enginesfastJet planesThrust reversersTestingfastThrust reversalnasatTurbofansnasatAeronautical engineeringnasatAircraft designnasatPerformance testsnasatAirplanesBrakes.AirplanesDesign and construction.AirplanesMotorsThrust.AirplanesTurbofan engines.Jet planesThrust reversersTesting.Thrust reversal.Turbofans.Aeronautical engineering.Aircraft design.Performance tests.Asbury Scott C.1397878Yetter Jeffery A.Langley Research Center,BUFBUFOCLCQOCLCFOCLCOOCLCQGPOBOOK9910707886903321Static performance of six innovative thrust reverser concepts for subsonic transport applications3460131UNINA