02155oam 2200529 450 991070420440332120160219102337.0(CKB)5470000002439635(OCoLC)74226211(EXLCZ)99547000000243963520080513j199705 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPerformance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /William T. Yeager, Jr. [and four others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,May 1997.1 online resource (23 pages) illustrationsNASA technical memorandum ;4754ARL technical report ;1283Title from title screen (viewed on Feb. 19, 2016)."May 1997.""Performing organizations: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center; Joint Research Program Office, Aeroflightdynamics Directorate, U.S. Army Aviation and Troop Command, NASA Langley Research Center"--Report documentation page."ATCOM technical report 97-A-006."Includes bibliographical references (page 6).Rotary wingsnasatVibratory loadsnasatTransonic wind tunnelsnasatPaddlesnasatRotorsnasatRotary wings.Vibratory loads.Transonic wind tunnels.Paddles.Rotors.Yeager William T.1398153Langley Research Center,United States.National Aeronautics and Space Administration,DTICEDTICEOCLCQGPOBOOK9910704204403321Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip3490132UNINA