02102nam 2200529I 450 991070561660332120170908153526.0(CKB)5470000002452234(OCoLC)988539972(EXLCZ)99547000000245223420170531j200306 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierOn the physics of flow separation along a low pressure turbine blade under unsteady flow conditions /Meinhard T. Schobeiri and Burak Öztürk, David E. AshpisCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,June 2003.1 online resource (16 pages) color illustrationsNASA/TM ;2003-212290"June 2003.""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.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field" Report documentation page."GT-2003-38917."Includes bibliographical references (pages 15-16).Boundary layersnasatLow pressurenasatTurbine bladesnasatTurbomachinerynasatTurbulent wakesnasatUnsteady flownasatBoundary layers.Low pressure.Turbine blades.Turbomachinery.Turbulent wakes.Unsteady flow.Schobeiri Meinhard1389884Öztürk BurakAshpis D. E(David E.),NASA Glenn Research Center,GPOGPOBOOK9910705616603321On the physics of flow separation along a low pressure turbine blade under unsteady flow conditions3441910UNINA