02346oam 2200601 450 991070013880332120140129154302.0(CKB)5470000002407580(OCoLC)707645081(EXLCZ)99547000000240758020110317g20102011 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierResults of an advanced fan stage operating over a wide range of speed and bypass ratio /Kenneth L. Suder [and five others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]-[2011]1 online resource (2 volumes) color illustrationsNASA/TM ;2010-216769, 2011-216769Title from title screen (viewed on Jan. 29, 2014)."Prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010."Includes bibliographical references.pt. 1. Fan stage design and experimental results -- pt 2. Comparison of CFD and experimental results.Aerodynamic stallingnasatBypass rationasatComputational fluid dynamicsnasatPropulsion system configurationsnasatTransonic compressorsnasatTurbofansnasatSupersonic speednasatComputerized simulationnasatAerodynamic stalling.Bypass ratio.Computational fluid dynamics.Propulsion system configurations.Transonic compressors.Turbofans.Supersonic speed.Computerized simulation.Suder Kenneth L(Kenneth Lee)1391483Fundamental Aeronautics Program (U.S.),NASA Glenn Research Center,ASME Turbo Expo(2010 :Glasgow, Scotland)GPOGPOGPOOCLCQGPOBOOK9910700138803321Results of an advanced fan stage operating over a wide range of speed and bypass ratio3445297UNINA