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001 9910700865303321
005 20110822150811.0
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035   $a(OCoLC)747503958
035   $a(EXLCZ)995470000002412363
100   $a20110822d2011      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical prediction of supersonic shock-boundary layer interaction$b[electronic resource] /$fVishal A. Bhagwandin and James DeSpirito
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2011]
215   $a1 online resource (viii, 36 pages) $ccolor illustrations
225 1 $aARL-TR ;$v5602
300   $aTitle from title screen (viewed on Aug. 19, 2011).
300   $a"July 2011."
320   $aIncludes bibliographical references (pages 32-33).
606   $aShock waves$xResearch
606   $aAerospace engineering$xResearch
615  0$aShock waves$xResearch.
615  0$aAerospace engineering$xResearch.
700   $aBhagwandin$b Vishal A$01420296
701   $aDeSpirito$b James$01400611
712 02$aU.S. Army Research Laboratory.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700865303321
996   $aNumerical prediction of supersonic shock-boundary layer interaction$93537693
997   $aUNINA