01930nam 2200517 450 991070585960332120170727103239.0(CKB)5470000002453820(OCoLC)995164631(EXLCZ)99547000000245382020170727j199806 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierMach number effects on turbine blade transition length prediction /R.J. Boyle and F.F. SimonCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,June 1998.1 online resource (12 pages) illustrationsNASA/TM ;1998-208404"June 1998.""Prepared for the Turbo Expo '98 sponsored by 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."98-GT-367."Includes bibliographical references (pages 11-12).Mach numbernasatTurbine bladesnasatMathematical modelsnasatTurbulence modelsnasatNavier-Stokes equationnasatBoundary layer transitionnasatMach number.Turbine blades.Mathematical models.Turbulence models.Navier-Stokes equation.Boundary layer transition.Boyle Robert J.1387461Simon F. F(Frederick F.),Lewis Research Center,GPOGPOBOOK9910705859603321Mach number effects on turbine blade transition length prediction3473392UNINA