LEADER 01462nam  2200421Ka 450 
001 9910698091103321
005 20090203095010.0
035   $a(CKB)5470000002394088
035   $a(OCoLC)301551370
035   $a(EXLCZ)995470000002394088
100   $a20090203d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aHigh speed corner and gap seal computations using an LU-SGS scheme$b[electronic resource] /$fWilliam J. Coirier
210  1$a[Washington, DC] :$cNational Aeronautics and Space Administration,$d[1989]
215   $a14 pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v102138
300   $aTitle from title screen (viewed Feb. 2, 2009)
606   $aAlgorithms$2nasat
606   $aEuler equations of motion$2nasat
606   $aGauss equation$2nasat
606   $aHypersonic flow$2nasat
606   $aNavier-Stokes equation$2nasat
615  7$aAlgorithms.
615  7$aEuler equations of motion.
615  7$aGauss equation.
615  7$aHypersonic flow.
615  7$aNavier-Stokes equation.
700   $aCoirier$b William John$f1962-$01408678
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910698091103321
996   $aHigh speed corner and gap seal computations using an LU-SGS scheme$93493147
997   $aUNINA