02047nam 2200541 a 450 991069692460332120230902162300.0(CKB)5470000002383649(OCoLC)642699029(EXLCZ)99547000000238364920100621d2009 ua 0engur|n|||||||||txtrdacontentcrdamediacrrdacarrierAxial and centrifugal compressor mean line flow analysis method[electronic resource] /Joseph P. Veres ; 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 (32 pages) illustrationsNASA TM- ;2009-215585Title from title screen (viewed on June 21, 2010)."November 2009.""AIAA-2009-1641."Includes bibliographical references (page 32).NASA technical memorandum ;2009-215585.TurbocompressorsnasatFluid flownasatComputational fluid dynamicsnasatCompressible fluidsnasatDesign analysisnasatGuide vanesnasatCentrifugal compressorsnasatTurbocompressors.Fluid flow.Computational fluid dynamics.Compressible fluids.Design analysis.Guide vanes.Centrifugal compressors.Veres Joseph P1386375NASA Glenn Research Center.AIAA Aerospace Sciences Meeting(47th :2009 :Orlando, Fla.)GPOGPOBOOK9910696924603321Axial and centrifugal compressor mean line flow analysis method3469597UNINA