LEADER 02102nam  2200529I  450 
001 9910705616603321
005 20170908153526.0
035   $a(CKB)5470000002452234
035   $a(OCoLC)988539972
035   $a(EXLCZ)995470000002452234
100   $a20170531j200306    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOn the physics of flow separation along a low pressure turbine blade under unsteady flow conditions /$fMeinhard T. Schobeiri and Burak O?ztu?rk, David E. Ashpis
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJune 2003.
215   $a1 online resource (16 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2003-212290
300   $a"June 2003."
300   $a"Prepared for the Turbo Expo 2003 cosponsored by the American Society of Mechanical Engineers and the International Gas Turbine Institute, Atlanta, Georgia, June 16-19, 2003."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field" Report documentation page.
300   $a"GT-2003-38917."
320   $aIncludes bibliographical references (pages 15-16).
606   $aBoundary layers$2nasat
606   $aLow pressure$2nasat
606   $aTurbine blades$2nasat
606   $aTurbomachinery$2nasat
606   $aTurbulent wakes$2nasat
606   $aUnsteady flow$2nasat
615  7$aBoundary layers.
615  7$aLow pressure.
615  7$aTurbine blades.
615  7$aTurbomachinery.
615  7$aTurbulent wakes.
615  7$aUnsteady flow.
700   $aSchobeiri$b Meinhard$01389884
702   $aO?ztu?rk$b Burak
702   $aAshpis$b D. E$g(David E.),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705616603321
996   $aOn the physics of flow separation along a low pressure turbine blade under unsteady flow conditions$93441910
997   $aUNINA