02111nam 2200541Ia 450 991070030230332120120106090608.0(CKB)5470000002409969(OCoLC)733291346(EXLCZ)99547000000240996920110628d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierEffects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan[electronic resource] /Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2011]1 online resource (14 pages) color illustrationsNASA/TM ;2011-216959Title from title screen (viewed on June 27, 2011)."January 2011.""AIAA-2010-6711."Includes bibliographical references (pages 13-14).AeroelasticitynasatTurbomachinerynasatTurbofansnasatComputational fluid dynamicsnasatInlet flownasatAerodynamic characteristicsnasatHigh speednasatAeroelasticity.Turbomachinery.Turbofans.Computational fluid dynamics.Inlet flow.Aerodynamic characteristics.High speed.Herrick Gregory Paul1972-1387242Fundamental Aeronautics Program (U.S.)NASA Glenn Research Center.AIAA/ASME/SAE/ASEE Joint Propulsion Conference(46th :2010 :Nashville, Tenn.)GPOGPOBOOK9910700302303321Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan3436840UNINA