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035   $a(CKB)5470000002393817
035   $a(OCoLC)299571518
035   $a(EXLCZ)995470000002393817
100   $a20090126d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMach 5 inlet CFD and experimental results$b[electronic resource] /$fLois J. Weir, and D. R. Reddy, and George D. Rupp
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$d[1989]
215   $a14 pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v102317
300   $aTitle from fitle screen (viewed Jan. 23, 2009)
517 3 $aMach five inlet computational fluid dynamics and experimental results
606   $aComputational fluid dynamics$2nasat
606   $aEngine inlets$2nasat
606   $aFlow distribution$2nasat
606   $aMach number$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aWind tunnel tests$2nasat
615  7$aComputational fluid dynamics.
615  7$aEngine inlets.
615  7$aFlow distribution.
615  7$aMach number.
615  7$aNavier-Stokes equation.
615  7$aWind tunnel tests.
700   $aWeir$b Lois J$01420759
701   $aReddy$b D. R$01420760
701   $aRupp$b George D$01420761
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910697917903321
996   $aMach 5 inlet CFD and experimental results$93539746
997   $aUNINA