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100   $a20100621d2009      ua             0
101 0 $aeng
135   $aur|n|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAxial and centrifugal compressor mean line flow analysis method$b[electronic resource] /$fJoseph P. Veres ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (32 pages) $cillustrations
225 1 $aNASA TM- ;$v2009-215585
300   $aTitle from title screen (viewed on June 21, 2010).
300   $a"November 2009."
300   $a"AIAA-2009-1641."
320   $aIncludes bibliographical references (page 32).
410  0$aNASA technical memorandum ;$v2009-215585.
606   $aTurbocompressors$2nasat
606   $aFluid flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aCompressible fluids$2nasat
606   $aDesign analysis$2nasat
606   $aGuide vanes$2nasat
606   $aCentrifugal compressors$2nasat
615  7$aTurbocompressors.
615  7$aFluid flow.
615  7$aComputational fluid dynamics.
615  7$aCompressible fluids.
615  7$aDesign analysis.
615  7$aGuide vanes.
615  7$aCentrifugal compressors.
700   $aVeres$b Joseph P$01386375
712 02$aNASA Glenn Research Center.
712 12$aAIAA Aerospace Sciences Meeting$d(47th :$f2009 :$eOrlando, Fla.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910696924603321
996   $aAxial and centrifugal compressor mean line flow analysis method$93469597
997   $aUNINA