02201nam 2200517 450 991070245330332120151124151616.0(CKB)5470000002427635(OCoLC)930297904(EXLCZ)99547000000242763520151124j201209 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierCFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /Samuel J. VinciCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,September 2012.1 online resource (xiv, 113 pages) color illustrationsNASA/CR ;2012-217417Title from title screen (viewed Nov. 24, 2015)."September 2012.""Performing organization: Cleveland State University"--Report documentation page."Prepared under NASA interagency agreement no. NNC07IA10I (through U.S. Navy Agreement No. N00189-07-P-A253)."Includes bibliographical references (pages 110-113).CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil Computational fluid dynamicsnasatPressure rationasatBoundary layersnasatFinite volume methodnasatLow speed wind tunnelsnasatComputational fluid dynamics.Pressure ratio.Boundary layers.Finite volume method.Low speed wind tunnels.Vinci Samuel J.1423048Cleveland State University.Fundamental Aeronautics Program (U.S.),NASA Glenn Research Center,GPOGPOBOOK9910702453303321CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report3549243UNINA