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100   $a20110131d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeroelastic computations of a compressor stage using the harmonic balance method$b[electronic resource] /$fT.S.R. Reddy, Milind A. Bakhle ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (22 pages) $cillustrations
225 1 $aNASA/TM ;$v2010-216240
300   $aTitle from title screen (viewed on Jan. 31, 2011).
300   $a"July 2010."
320   $aIncludes bibliographical references (pages 21-22).
606   $aAeroelasticity$2nasat
606   $aBalance$2nasat
606   $aCompressors$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aHarmonic analysis$2nasat
606   $aThree dimensional models$2nasat
606   $aTransonic compressors$2nasat
615  7$aAeroelasticity.
615  7$aBalance.
615  7$aCompressors.
615  7$aComputational fluid dynamics.
615  7$aHarmonic analysis.
615  7$aThree dimensional models.
615  7$aTransonic compressors.
700   $aReddy$b T. S. R$01400944
701   $aBakhle$b Milind A$01401182
712 02$aNASA Glenn Research Center.
712 12$aJoint Propulsion Conference and Exhibit$d(45th :$f2009 :$eDenver, Colo.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699644203321
996   $aAeroelastic computations of a compressor stage using the harmonic balance method$93507655
997   $aUNINA