02086nam 2200565 a 450 991070195000332120121101145647.0(CKB)5470000002422618(OCoLC)815659970(EXLCZ)99547000000242261820121101d2012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierExhaust nozzle plume effects on sonic boom test results for vectored nozzles[electronic resource] /Raymond CastnerCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (16 pages) color illustrationsNASA/TM ;2012-217229Title from title screen (viewed on Nov. 1, 2012)."February 2012.""Prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE,San Diego, California, July 31-August 3, 2011.""AIAA-2011-5974."Includes bibliographical references (pages 15-16).Exhaust nozzlesnasatSonic boomsnasatComputational fluid dynamicsnasatElastic wavesnasatPlumesnasatF-15 aircraftnasatSupersonic aircraftnasatPressure rationasatExhaust nozzles.Sonic booms.Computational fluid dynamics.Elastic waves.Plumes.F-15 aircraft.Supersonic aircraft.Pressure ratio.Castner Raymond S1392322NASA Glenn Research Center.Joint Propulsion Conference and Exhibit(47th :2011 :San Diego, Calif.)GPOGPOBOOK9910701950003321Exhaust nozzle plume effects on sonic boom test results for vectored nozzles3546377UNINA