02315nam 2200589 450 991070618480332120170821140007.0(CKB)5470000002454576(OCoLC)1001438248(EXLCZ)99547000000245457620170821j199901 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPrediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn /David L. RigbyCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,January 1999.1 online resource (12 pages) illustrationsNASA/TM ;1999-208501"January 1999.""Prepared for the 43rd Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (pages 11-12).Reynolds averagingnasatComputational fluid dynamicsnasatNavier-Stokes equationnasatTurbine bladesnasatCooling systemsnasatMass transfernasatHeat transfernasatK-omega turbulence modelnasatEngine coolantsnasatComputational gridsnasatReynolds averaging.Computational fluid dynamics.Navier-Stokes equation.Turbine blades.Cooling systems.Mass transfer.Heat transfer.K-omega turbulence model.Engine coolants.Computational grids.Rigby D. L(David Lester),1963-1414359Lewis Research Center,GPOGPOBOOK9910706184803321Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn3546179UNINA