01977oam 2200517I 450 991070700930332120160405153305.0(CKB)5470000002461399(OCoLC)703662716(EXLCZ)99547000000246139920110224j199611 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFlight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests /Jon K. Holzman, Lannie D. Webb, and Frank W. Burcham, JrEdwards, California.:National Aeronautics and Space Administration, Dryden Flight Research Center,November 1996.1 online resource (iv, 26 pages) illustrationsNASA technical memorandum ;104326Title from title screen (viewed April 5, 2016)."November 1996.""Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.Includes bibliographical references (page 26).Acoustic measurementnasatAircraft noisenasatEngine noisenasatExhaust gasesnasatJet enginesnasatAcoustic measurement.Aircraft noise.Engine noise.Exhaust gases.Jet engines.Holzman Jon K.1404714Webb Lannie D.Burcham Frank W.NASA Dryden Flight Research Center,United States.National Aeronautics and Space Administration,SSNSSNGPOBOOK9910707009303321Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests3479818UNINA