02149nam 2200589Ia 450 991070157400332120120326134904.0(CKB)5470000002419346(OCoLC)781638890(EXLCZ)99547000000241934620120326d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierDevelopment of an open rotor cycle model in NPSS using a multi-design point approach[electronic resource] /Eric S. HendericksCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2011]1 online resource (13 pages) illustrations (some color)NASA/TM ;2011-217225Title from title screen (viewed on Mar. 26, 2012)."October 2011.""Prepared for the Turbo Expo 2011 sponsored by the American Society of Mechanical Engineers (ASME) Vancouver, British Columbia, Canada, June 6-10, 2011.""GT2011-46694."Includes bibliographical references (page 13).Contrarotating propellersnasatTurbinesnasatExhaust emissionnasatFlight envelopesnasatPropeller bladesnasatPropeller efficiencynasatTakeoffnasatAerodynamicsnasatFuel consumptionnasatContrarotating propellers.Turbines.Exhaust emission.Flight envelopes.Propeller blades.Propeller efficiency.Takeoff.Aerodynamics.Fuel consumption.Hendricks Eric S1402593NASA Glenn Research Center.ASME Turbo Expo(2011 :Vancouver, B.C.)GPOGPOBOOK9910701574003321Development of an open rotor cycle model in NPSS using a multi-design point approach3486112UNINA