LEADER 01972nam  2200577 a 450 
001 9910702003503321
005 20120918092807.0
035   $a(CKB)5470000002424098
035   $a(OCoLC)810135701
035   $a(EXLCZ)995470000002424098
100   $a20120918d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aReacting multi-species gas capability for USM3D flow solver$b[electronic resource] /$fNeal T. Frink and David M. Schuster
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2012]
215   $a1 online resource (78 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217575
300   $aTitle from title screen (viewed on Sept. 18, 2012).
300   $a"May 2012."
300   $a"NASA Engineering and Safety Center."
300   $a"NESC-RP-07-037."
320   $aIncludes bibliographical references (page 47).
606   $aNavier-Stokes equation$2nasat
606   $aSafety$2nasat
606   $aLaunch vehicles$2nasat
606   $aGas flow$2nasat
606   $aHigh temperature gases$2nasat
606   $aTemperature effects$2nasat
606   $aJet impingement$2nasat
606   $aAres 1 launch vehicle$2nasat
615  7$aNavier-Stokes equation.
615  7$aSafety.
615  7$aLaunch vehicles.
615  7$aGas flow.
615  7$aHigh temperature gases.
615  7$aTemperature effects.
615  7$aJet impingement.
615  7$aAres 1 launch vehicle.
700   $aFrink$b Neal T$01413983
701   $aSchuster$b D. M$g(David M.)$01413984
712 02$aNASA Engineering and Safety Center.
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702003503321
996   $aReacting multi-species gas capability for USM3D flow solver$93511847
997   $aUNINA