02142nam 2200577 a 450 991070191210332120120830112334.0(CKB)5470000002423001(OCoLC)808726339(EXLCZ)99547000000242300120120830d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierExhaust nozzle plume effects on sonic boom test results for isolated nozzles[electronic resource] /Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2011]1 online resource (16 pages) color illustrationsNASA/TM ;2011-217137Title from title screen (viewed on Aug. 30, 2012)."December 2011.""AIAA-2010-4936."Includes bibliographical references (page 16).Exhaust nozzlesnasatNozzle flownasatPlumesnasatSupersonic aircraftnasatComputational fluid dynamicsnasatNozzle geometrynasatPressure rationasatShock wavesnasatElastic wavesnasatExhaust nozzles.Nozzle flow.Plumes.Supersonic aircraft.Computational fluid dynamics.Nozzle geometry.Pressure ratio.Shock waves.Elastic waves.Castner Raymond S1392322NASA Glenn Research Center.AIAA Applied Aerodynamics Conference(18th :2010 :Chicago, Ill.)GPOGPOBOOK9910701912103321Exhaust nozzle plume effects on sonic boom test results for isolated nozzles3518430UNINA