02086nam 2200541I 450 991070243170332120140709095534.0(CKB)5470000002427854(OCoLC)883208686(EXLCZ)99547000000242785420140709j201308 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierUpdated assessment of an open rotor airplane using an advanced blade design /Eric S. Hendricks [and four others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,August 2013.1 online resource (13 pages) color illustrationsNASA/TM ;2013-218074Title from title screen (viewed July 9, 2014)."August 2013.""Prepared for the 49th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE San Jose, California, July 14-17, 2013.""AIAA-2013-3628."Includes bibliographical references (pages 12-13).Contrarotating propellersnasatFuel consumptionnasatLow noisenasatNoise intensitynasatNoise prediction (aircraft)nasatPropulsion system configurationsnasatPropulsion system performancenasatContrarotating propellers.Fuel consumption.Low noise.Noise intensity.Noise prediction (aircraft)Propulsion system configurations.Propulsion system performance.Hendricks Eric S.1402593NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702431703321Updated assessment of an open rotor airplane using an advanced blade design3473451UNINA