02188nam 2200589 a 450 991069954850332120230902161548.0(CKB)5470000002403442(OCoLC)669025050(EXLCZ)99547000000240344220101007d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierSlot nozzle effects for reduced sonic boom on a generic supersonic wing section[electronic resource] /Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (10 pages) illustrationsNASA TM- ;2010-216258Title from title screen (viewed on Oct. 7, 2010)."March 2010.""AIAA-2010-1386."Includes bibliographical references (page 10)NASA technical memorandum ;216258.Exhaust nozzlesnasatSonic boomsnasatWing slotsnasatAircraft controlnasatComputational fluid dynamicsnasatExhaust gasesnasatSupersonic speednasatMach numbernasatHigh aspect rationasatExhaust nozzles.Sonic booms.Wing slots.Aircraft control.Computational fluid dynamics.Exhaust gases.Supersonic speed.Mach number.High aspect ratio.Castner Raymond S1392322NASA Glenn Research Center.AIAA Aerospace Sciences Meeting(48th :2010 :Orlando, Fla.)GPOGPOBOOK9910699548503321Slot nozzle effects for reduced sonic boom on a generic supersonic wing section3455185UNINA