01615nam 2200469I 450 991070571390332120170707085648.0(CKB)5470000002453272(OCoLC)992989283(EXLCZ)99547000000245327220170707j201705 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierInlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility /Richard F. BozakCleveland, Ohio:National Aeronautics and Space Administration, Glenn Research Center,May 2017.1 online resource (6 pages) color illustrationsNASA/TM ;2017-219489"May 2017."Includes bibliographical references (page 2).Acoustic propertiesnasatAerodynamic characteristicsnasatBypass rationasatNoise reductionnasatRotorsnasatTurbofan enginesnasatAcoustic properties.Aerodynamic characteristics.Bypass ratio.Noise reduction.Rotors.Turbofan engines.Bozak Richard F.1405259NASA Glenn Research Center,GPOGPOBOOK9910705713903321Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility3494649UNINA