02020nam 2200553 450 991070243670332120140709114120.0(CKB)5470000002427803(OCoLC)883215359(EXLCZ)99547000000242780320140709j201312 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /Christopher E. Hughes [and three others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,December 2013.1 online resource (35 pages) illustrations (some color)NASA/TM ;2013-214029Title from title screen (viewed July 9, 2014)."December 2013.""GT2005-68573."Includes bibliographical references (page 13).AeroacousticsnasatAerodynamic characteristicsnasatAerodynamic noisenasatAircraft noisenasatFan bladesnasatFar fieldsnasatLaser doppler velocimetersnasatLow speed wind tunnelsnasatAeroacoustics.Aerodynamic characteristics.Aerodynamic noise.Aircraft noise.Fan blades.Far fields.Laser doppler velocimeters.Low speed wind tunnels.Hughes Christopher E.1402594NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702436703321The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator3489728UNINA