LEADER 01781oam  2200493Ka 450 
001 9910698882803321
005 20090507084624.0
035   $a(CKB)5470000002397034
035   $a(OCoLC)320429045
035   $a(OCoLC)995470000002397034
035   $a(EXLCZ)995470000002397034
100   $a20090507d1988      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDuct flow nonuniformities$b[electronic resource] $eeffects of struts in SSME HGM II? : interim report /$fprepared for National Aeronautics and Space Administration, Marshall Space Flight Center, by Roger Burke
210  1$aHuntsville, AL :$cLockheed Missiles & Space Company, Inc., Huntsville Engineering Center ;$aMarshall Space Flight Center, AL :$cNational Aeronautics and Space Administration,$d[1988]
215   $a1 volume
225 1 $aNASA CR ;$v179285
300   $aTitle from title screen (viewed May 6, 2009)
517   $aDuct flow nonuniformities 
606   $aComputational fluid dynamics$2nasat
606   $aLaminar flow$2nasat
606   $aMathematical models$2nasat
606   $aSpace Shuttle Main Engine$2nasat
606   $aStruts$2nasat
606   $aTurbulent flow$2nasat
615  7$aComputational fluid dynamics.
615  7$aLaminar flow.
615  7$aMathematical models.
615  7$aSpace Shuttle Main Engine.
615  7$aStruts.
615  7$aTurbulent flow.
700   $aBurke$b Roger$01387073
712 02$aHuntsville Engineering Center.
712 02$aGeorge C. Marshall Space Flight Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910698882803321
996   $aDuct flow nonuniformities$93504240
997   $aUNINA