LEADER 01872nam  2200481I  450 
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005 20160202162800.0
035   $a(CKB)5470000002438896
035   $a(OCoLC)936387373
035   $a(EXLCZ)995470000002438896
100   $a20160202j201509    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction /$fDavid O. Davis
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dSeptember 2015.
215   $a1 online resource (13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218841
300   $aTitle from title screen (viewed on Feb. 2, 2016).
300   $a"September 2015."
300   $a"Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015
320   $aIncludes bibliographical references (page 13).
517 3 $aComputational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction
606   $aBoundary layers$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aShock wave interaction$2nasat
606   $aFlow measurement$2nasat
606   $aTurbulent flow$2nasat
615  7$aBoundary layers.
615  7$aComputational fluid dynamics.
615  7$aShock wave interaction.
615  7$aFlow measurement.
615  7$aTurbulent flow.
700   $aDavis$b David O.$01402770
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704277603321
996   $aCFD validation experiment of a Mach 2.5 axisymmetric shock-wave$93500659
997   $aUNINA