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001 9910707311303321
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035   $a(CKB)5470000002464409
035   $a(OCoLC)844689779
035   $a(EXLCZ)995470000002464409
100   $a20130526j199611    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct /$fMilo D. Dahl
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dNovember 1996.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107358
300   $aTitle from title screen (viewed Aug. 2, 2016).
300   $a"November 1996"--Report documentation page.
300   $a"Prepared for the International Mechanical Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 11-12).
606   $aSupersonic jet flow$2nasat
606   $aDucts$2nasat
606   $aDucted flow$2nasat
606   $aDuct geometry$2nasat
606   $aCircles (geometry)$2nasat
606   $aBoundary conditions$2nasat
606   $aKelvin-Helmholtz instability$2nasat
606   $aSupersonic inlets$2nasat
615  7$aSupersonic jet flow.
615  7$aDucts.
615  7$aDucted flow.
615  7$aDuct geometry.
615  7$aCircles (geometry)
615  7$aBoundary conditions.
615  7$aKelvin-Helmholtz instability.
615  7$aSupersonic inlets.
700   $aDahl$b Milo D.$f1956-$01397975
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707311303321
996   $aThe effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct$93497084
997   $aUNINA