02124oam 2200649I 450 991070616930332120170825125338.0(CKB)5470000002454732(OCoLC)858255342(EXLCZ)99547000000245473220130912j199905 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierAeroacoustic data for a high Reynolds number axisymmetric subsonic jet /Michael K. Ponton, Lawrence S. Ukeiley, Sang W. LeeHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,May 1999.1 online resource (84 pages) illustrationsNASA/TM ;1999-209336"May 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 5).AeroacousticsnasatConvergent nozzlesnasatJet flownasatSubsonic flownasatHigh Reynolds numbernasatPressure oscillationsnasatFlow characteristicsnasatEngine noisenasatExhaust nozzlesnasatExhaust gasesnasatAeroacoustics.Convergent nozzles.Jet flow.Subsonic flow.High Reynolds number.Pressure oscillations.Flow characteristics.Engine noise.Exhaust nozzles.Exhaust gases.Ponton Michael K.1416815Ukeiley Lawrence S.Lee Sang W.Langley Research Center,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706169303321Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet3523467UNINA