01991oam 2200541I 450 991070730640332120160803155607.0(CKB)5470000002464459(OCoLC)844685565(EXLCZ)99547000000246445920130526j199801 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads /Matthew L. Wilbur [and four others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,January 1998.1 online resource (247 pages) illustrationsNASA/TM ;1998-206281ARL-TR ;1401Title from title screen (viewed Aug. 3, 2016)."January 1998.""Performing organization: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 5).HelicoptersnasatLoads (forces)nasatRotary wing aircraftnasatRotor dynamicsnasatWind tunnel testsnasatHelicopters.Loads (forces)Rotary wing aircraft.Rotor dynamics.Wind tunnel tests.Wilbur Matthew L.1389368Langley Research Center,Vehicle Technology Center (U.S. Army Research Laboratory),OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910707306403321Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads3440835UNINA