01963oam 2200565 450 991070730810332120160803134744.0(CKB)5470000002464442(OCoLC)844683682(EXLCZ)99547000000246444220130526j199612 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of wake passing on turbine blade film cooling /James David HeidmannCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,December 1996.1 online resource (xvii, 248 pages) illustrationsNASA technical memorandum ;107380Title from title screen (viewed Aug. 3, 2016)."December 1996.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (pages 244-248).Turbine bladesnasatFilm coolingnasatWakesnasatNavier-Stokes equationnasatComputational fluid dynamicsnasatTurbomachinerynasatFlow distributionnasatUnsteady aerodynamicsnasatTurbine blades.Film cooling.Wakes.Navier-Stokes equation.Computational fluid dynamics.Turbomachinery.Flow distribution.Unsteady aerodynamics.Heidmann James D.1407008Lewis Research Center,OCLCEOCLCEOCLCQGPOBOOK9910707308103321The effect of wake passing on turbine blade film cooling3487269UNINA