LEADER 01893nam  2200493I  450 
001 9910704031603321
005 20151030161002.0
035   $a(CKB)5470000002437340
035   $a(OCoLC)927176907
035   $a(EXLCZ)995470000002437340
100   $a20151030j198507    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUse of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations / Yehia M. Rizk, Joseph L. Steger, Denny S. Chausse
210  1$aMoffett Field, CA :$cNational Aeronautics and Space Administration, Ames Research Center,$dJuly 1985.
215   $a1 online resource (13 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v86776
300   $aTitle from title screen (viewed Oct. 30, 2015).
300   $a"July 1985."
320   $aIncludes bibliographical references (page 7).
606   $aComputational grids$2nasat
606   $aGrid generation (mathematics)$2nasat
606   $aSpace Shuttle orbiters$2nasat
606   $aSupersonic flow$2nasat
606   $aAerodynamic configurations$2nasat
615  7$aComputational grids.
615  7$aGrid generation (mathematics)
615  7$aSpace Shuttle orbiters.
615  7$aSupersonic flow.
615  7$aAerodynamic configurations.
700   $aRizk$b Yehia M.$01395177
702   $aSteger$b Joseph L.
702   $aChausse$b Denny S.
712 02$aAmes Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704031603321
996   $aUse of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations$93453244
997   $aUNINA