02324nam 2200613 a 450 991069954710332120230902162153.0(CKB)5470000002403456(OCoLC)669000975(EXLCZ)99547000000240345620101007d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierWind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles[electronic resource] /Raymond S. Castner ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (10 pages) illustrationsNASA TM- ;2010-216259Title from title screen (viewed on Oct. 7, 2010)."April 2010.""AIAA-2009-5369."Includes bibliographical references (page 10)NASA technical memorandum ;216259.Wind tunnel testsnasatSupersonic aircraftnasatAerodynamic configurationsnasatLow costnasatSupersonic wind tunnelsnasatWind tunnel modelsnasatSonic boomsnasatStatic pressurenasatPressure sensorsnasatExhaust nozzlesnasatWind tunnel tests.Supersonic aircraft.Aerodynamic configurations.Low cost.Supersonic wind tunnels.Wind tunnel models.Sonic booms.Static pressure.Pressure sensors.Exhaust nozzles.Castner Raymond S1392322NASA Glenn Research Center.Joint Propulsion Conference and Exhibit(45th :2009 :Denver, Colo.)GPOGPOBOOK9910699547103321Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles3485459UNINA