02059nam 2200517 450 991070730900332120160803115058.0(CKB)5470000002464432(OCoLC)954593999(EXLCZ)99547000000246443220160803j199611 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPredicted turbine heat transfer for a range of test conditions /R.J. Boyle and B.L. LucciCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,November 1996.1 online resource (16 pages) illustrationsNASA technical memorandum ;107374Title from title screen (viewed Aug. 3, 2016)."November 1996"--Report documentation page."Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (page 16).Aerodynamic characteristicsnasatHeat transfernasatTurbulence modelsnasatTurbine bladesnasatWall flownasatNavier-Stokes equationnasatAerodynamic characteristics.Heat transfer.Turbulence models.Turbine blades.Wall flow.Navier-Stokes equation.Boyle Robert J.1387461Lucci Barbara L.Lewis Research Center,GPOGPOBOOK9910707309003321Predicted turbine heat transfer for a range of test conditions3437387UNINA