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035   $a(CKB)5470000002434028
035   $a(OCoLC)910630220
035   $a(EXLCZ)995470000002434028
100   $a20150603j201412    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAssessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods /$fGregory P. Herrick
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2014.
215   $a1 online resource (17 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218447
300   $aTitle from title screen (viewed on June 3, 2015).
300   $a"December 2014."
300   $a"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
320   $aIncludes bibliographical references (pages 15-17).
606   $aTurbomachinery$2nasat
606   $aFlutter analysis$2nasat
606   $aInlet flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aAeroelasticity$2nasat
615  7$aTurbomachinery.
615  7$aFlutter analysis.
615  7$aInlet flow.
615  7$aComputational fluid dynamics.
615  7$aAeroelasticity.
700   $aHerrick$b Gregory Paul$f1972-$01387242
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703769103321
996   $aAssessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods$93457802
997   $aUNINA