02108oam 2200553I 450 991070243180332120140709110119.0(CKB)5470000002427853(OCoLC)883213082(EXLCZ)99547000000242785320140709j201308 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /Ashlie B. McVetta, Paul W. Giel, Gerard E. WelchCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,August 2013.1 online resource (18 pages) color illustrationsNASA/TM ;2013-218070Title from title screen (viewed July 9, 2014)."August 2013.""Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 29-August 1, 2012.""AIAA-2012-3879."Includes bibliographical references (page 18).Aerodynamic heat transfernasatComputational fluid dynamicsnasatFlow measurementnasatInlet flownasatSupersonic turbinesnasatTurbine bladesnasatAerodynamic heat transfer.Computational fluid dynamics.Flow measurement.Inlet flow.Supersonic turbines.Turbine blades.McVetta Ashlie B.1396822Giel P. W(Paul W.),Welch Gerard E.NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOGPOBOOK9910702431803321Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade3457602UNINA