02339nam 2200613I 450 991070265610332120141202152004.0(CKB)5470000002429627(OCoLC)897217438(EXLCZ)99547000000242962720141202j201406 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /Ashlie B. McVetta, Paul W. Giel, Gerard E. WelchRevised copy.Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,June 2014.1 online resource (23 pages) color illustrationsNASA/TM ;2013-218070/REV1Title from title screen (viewed Dec. 1, 2014)."June 2014.""This revised copy, numbered as NASA/TM-2013-218070/REV1, June 2014, supersedes the previous version, NASA/TM-2013-218070, August 2013, in its entirety.""AIAA-2012-3879."Includes bibliographical references (page 23).Supersonic turbinesnasatTurbine bladesnasatAerodynamic heat transfernasatComputational fluid dynamicsnasatReynolds numbernasatPressure distributionnasatInlet flownasatAngles (geometry)nasatSupersonic turbines.Turbine blades.Aerodynamic heat transfer.Computational fluid dynamics.Reynolds number.Pressure distribution.Inlet flow.Angles (geometry)McVetta Ashlie B.1396822Giel P. W(Paul W.),Welch Gerard E.NASA Glenn Research Center,United States.National Aeronautics and Space Administration,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910702656103321Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade3457602UNINA