01944nam 2200529I 450 991069507180332120170912111821.0(CKB)5470000002366000(OCoLC)1003322880(EXLCZ)99547000000236600020170912j199111 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage /reported by M.F. BlairEast Hartford, Connecticut :United Technologies Research Center,November 1991.1 online resource (vi, 67 pages, 172 unnumbered pages) illustrationsNASA CR ;184260"November 1991."Description based on online resource; title from PDF title page (NASA, viewed Sep. 12, 2017).Includes bibliographical references (pages 53-57).AerodynamicsnasatGas turbinesnasatHeat transfernasatRotorsnasatThree dimensional flownasatTurbine pumpsnasatTurbulence modelsnasatViscous flownasatAerodynamics.Gas turbines.Heat transfer.Rotors.Three dimensional flow.Turbine pumps.Turbulence models.Viscous flow.Blair M. F.1391724United Technologies Research Center,GPOGPOBOOK9910695071803321The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage3486471UNINA