02201nam 2200589 450 991070211380332120130115150042.0(CKB)5470000002425004(OCoLC)824456134(EXLCZ)99547000000242500420130115d2012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierImplementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade /Ali A. AmeriCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (25 pages) illustrations[NASA contractor report] ;NASA-CR 2012-217436Title from title screen (viewed Jan. 15, 2013)."April 2012.""This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."Includes bibliographical references (pages 24-25).Computational fluid dynamicsnasatTurbulent boundary layernasatTurbine bladesnasatHeat transfernasatLossesnasatLow Reynolds numbernasatPressure rationasatThree dimensional flownasatLaminar flownasatComputational fluid dynamics.Turbulent boundary layer.Turbine blades.Heat transfer.Losses.Low Reynolds number.Pressure ratio.Three dimensional flow.Laminar flow.Ameri Ali A.1384587NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702113803321Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade3511555UNINA