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035   $a(CKB)5470000002454732
035   $a(OCoLC)858255342
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100   $a20130912j199905    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeroacoustic data for a high Reynolds number axisymmetric subsonic jet /$fMichael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1999.
215   $a1 online resource (84 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209336
300   $a"May 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
606   $aAeroacoustics$2nasat
606   $aConvergent nozzles$2nasat
606   $aJet flow$2nasat
606   $aSubsonic flow$2nasat
606   $aHigh Reynolds number$2nasat
606   $aPressure oscillations$2nasat
606   $aFlow characteristics$2nasat
606   $aEngine noise$2nasat
606   $aExhaust nozzles$2nasat
606   $aExhaust gases$2nasat
615  7$aAeroacoustics.
615  7$aConvergent nozzles.
615  7$aJet flow.
615  7$aSubsonic flow.
615  7$aHigh Reynolds number.
615  7$aPressure oscillations.
615  7$aFlow characteristics.
615  7$aEngine noise.
615  7$aExhaust nozzles.
615  7$aExhaust gases.
700   $aPonton$b Michael K.$01416815
702   $aUkeiley$b Lawrence S.
702   $aLee$b Sang W.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706169303321
996   $aAeroacoustic data for a high Reynolds number axisymmetric subsonic jet$93523467
997   $aUNINA