02291nam 2200601 a 450 991069690770332120230902161946.0(CKB)5470000002383819(OCoLC)640126883(EXLCZ)99547000000238381920100611d2009 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierLarge eddy simulation of transonic flow field in NASA rotor 37[electronic resource] /Chunill Hah ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2009]1 online resource (18 pages) illustrationsNASA TM- ;2009-215627Title from title screen (viewed on June 11, 2010)."September 2009."Includes bibliographical references (pages 6-7).NASA technical memorandum ;2009-215627.Transonic compressorsnasatPressure distributionnasatLarge eddy simulationnasatNavier-Stokes equationnasatComputational fluid dynamicsnasatFlow characteristicsnasatReynolds averagingnasatSeparated flownasatTurbulent flownasatBoundary layer separationnasatTransonic compressors.Pressure distribution.Large eddy simulation.Navier-Stokes equation.Computational fluid dynamics.Flow characteristics.Reynolds averaging.Separated flow.Turbulent flow.Boundary layer separation.Hah C1414468NASA Glenn Research Center.AIAA Aerospace Sciences Meeting(47th :2009 :Orlando, Fla.)GPOGPOBOOK9910696907703321Large eddy simulation of transonic flow field in NASA rotor 373521723UNINA