02082nam 2200517Ia 450 991070037140332120110628102118.0(CKB)5470000002409271(OCoLC)733290891(EXLCZ)99547000000240927120110628d2010 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierEffects of gas turbine component performance on engine and rotary wing vehicle size and performance[electronic resource] /Christopher A. Snyder, Douglas R. Thurman ; prepared for the 66th Annual Forum and Technology Display (AHS Forum 66) sponsored by the American Helicopter Society, Phoenix, Arizona, May 11-13, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (11 pages) color illustrationsNASA/TM ;2010-216907Title from title screen (viewed on June 27, 2011)."November 2010."Includes bibliographical references (page 11).Tilt rotor aircraftnasatGas turbine enginesnasatComponent reliabilitynasatWeight analysisnasatRotary wingsnasatFuel consumptionnasatTilt rotor aircraft.Gas turbine engines.Component reliability.Weight analysis.Rotary wings.Fuel consumption.Herrick Gregory Paul1972-1387242Thurman Douglas R1391713NASA Glenn Research Center.U.S. Army Research Laboratory.AHS Forum and Technology Display(66th :2010 :Phoenix, Ariz.)GPOGPOBOOK9910700371403321Effects of gas turbine component performance on engine and rotary wing vehicle size and performance3550969UNINA