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100   $a20170612j201612    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPassive rocket diffuser testing $ereacting flow performance of four second-throat geometries /$fDaniel R. Jones, Daniel C. Allgood, Grady P. Saunders
210  1$a[Stennis Space Center, Mississippi] :$cNational Aeronautics and Space Administration, [Stennis Space Center],$dDecember 2016.
215   $a1 online resource (26 pages) $ccolor illustrations
225 1 $aNASA technical memorandum ;$v2016-219221
300   $a"December 2016."
300   $a"The experimentation presented in this paper was carried out at SSC between May and August 2015" Page 3.
320   $aIncludes bibliographical references (pages 25-26).
517   $aPassive rocket diffuser testing 
606   $aBoundary layer separation$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aFlow distribution$2nasat
606   $aPressure effects$2nasat
606   $aPressure measurement$2nasat
606   $aRocket engines$2nasat
615  7$aBoundary layer separation.
615  7$aComputational fluid dynamics.
615  7$aFlow distribution.
615  7$aPressure effects.
615  7$aPressure measurement.
615  7$aRocket engines.
700   $aJones$b Daniel R.$01411498
702   $aAllgood$b Daniel C.
702   $aSaunders$b Grady P.
712 02$aJohn C. Stennis Space Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705789603321
996   $aPassive rocket diffuser testing$93502901
997   $aUNINA