LEADER 01882oam 2200505Ia 450 001 9910701830703321 005 20120615133651.0 035 $a(CKB)5470000002421803 035 $a(OCoLC)795582297 035 $a(EXLCZ)995470000002421803 100 $a20120615d1986 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aApplication of a Runge-Kutta scheme for high-speed inviscid internal flows$b[electronic resource] /$fAnutosh Moitra, Eli Turkel, Ajay Kumar 210 1$aHampton, Va. :$cInstitute for Computer Applications in Science and Engineering, NASA Langley Research Center$cUniversities Space Research Association,$d[1986] 215 $a1 online resource (i, 24 pages) $cillustrations 225 1 $aNASA contractor report ;$v178053 225 1 $aICASE report ;$vno. 86-5 300 $aTitle from title screen (viewed on June 15, 2012). 300 $a"January 1986." 320 $aIncludes bibliographical references (page 14). 606 $aComputational fluid dynamics$2nasat 606 $aInviscid flow$2nasat 606 $aRunge-Kutta method$2nasat 606 $aSupersonic flow$2nasat 615 7$aComputational fluid dynamics. 615 7$aInviscid flow. 615 7$aRunge-Kutta method. 615 7$aSupersonic flow. 700 $aMoitra$b Anutosh$01393816 701 $aTurkel$b E$01393817 701 $aKumar$b Ajay$0950772 712 02$aInstitute for Computer Applications in Science and Engineering. 712 02$aUniversities Space Research Association. 712 02$aLangley Research Center. 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910701830703321 996 $aApplication of a Runge-Kutta scheme for high-speed inviscid internal flows$93450389 997 $aUNINA