02045nam 2200553Ia 450 991069692940332120230902161942.0(CKB)5470000002383600(OCoLC)642331797(EXLCZ)99547000000238360020100618d2009 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierBroadband shock noise in internally-mixed dual-stream jets[electronic resource] /James E. Bridges ; prepared for the 15th Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) cosponsored by AIAA and CEAS, Miami, Florida, May 11-13, 2009Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2009]1 online resource (17 pages) illustrationsNASA TM- ;2009-215817Title from title screen (viewed on June 17, 2010)."November 2009.""AIAA-2009-3210."Includes bibliographical references (page 17).NASA technical memorandum ;2009-215817.Aerodynamic noisenasatNozzle flownasatNoise measurementnasatFlow noisenasatShock wavesnasatBypass rationasatShear layersnasatAerodynamic noise.Nozzle flow.Noise measurement.Flow noise.Shock waves.Bypass ratio.Shear layers.Bridges James E1394301NASA Glenn Research Center.AIAA/CEAS Aeroacoustics Conference(15th :2009 :Miami, Fla.)AIAA Aeroacoustics Conference(30th :2009 :Miami, Fla.)GPOGPOBOOK9910696929403321Broadband shock noise in internally-mixed dual-stream jets3451473UNINA