LEADER 01993nam  2200505I  450 
001 9910702430903321
005 20141203130447.0
035   $a(CKB)5470000002427862
035   $a(OCoLC)897378500
035   $a(EXLCZ)995470000002427862
100   $a20141203j201310    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUnderstanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses /$fDavid J. Friedlander
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2013.
215   $a1 online resource (xvi, 105 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-218081
300   $aTitle from title screen (viewed on Dec. 3, 2014).
300   $a"October 2013."
320   $aIncludes bibliographical references (pages 58-63).
517 3 $aUnderstanding the flow physics of shock boundary layer interactions using Computational Fluid Dynamics and numerical analyses
606   $aComputational fluid dynamics$2nasat
606   $aShock wave interaction$2nasat
606   $aBoundary layers$2nasat
606   $aFlow distribution$2nasat
606   $aParticle image velocimetry$2nasat
606   $aLarge eddy simulation$2nasat
615  7$aComputational fluid dynamics.
615  7$aShock wave interaction.
615  7$aBoundary layers.
615  7$aFlow distribution.
615  7$aParticle image velocimetry.
615  7$aLarge eddy simulation.
700   $aFriedlander$b David J.$01398592
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702430903321
996   $aUnderstanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses$93473449
997   $aUNINA