02032nam 2200529I 450 991070420510332120160218115134.0(CKB)5470000002439628(OCoLC)939619632(EXLCZ)99547000000243962820160218j199706 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierRotating shake test and modal analysis of a model helicopter rotor blade /W. Keats Wilkie, Paul H. Mirick, and Chester W. LangstonHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,June 1997.1 online resource (15 pages.) illustrationsNASA technical memorandum ;4760Title from title screen (viewed on Feb. 18, 2016)."June 1997.""Performing organizations: NASA Langley Research Center, Hampton, VA [and] Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton, VA"--Report documentation page."ARL technical report 1389."Includes bibliographical references (page 15).Rotary wingsnasatHelicoptersnasatAeroelasticitynasatHoveringnasatTorsionnasatRotary wings.Helicopters.Aeroelasticity.Hovering.Torsion.Wilkie W. Keats1410623Mirick Paul H.Langston Chester W.Vehicle Technology Center (U.S. Army Research Laboratory)Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910704205103321Rotating shake test and modal analysis of a model helicopter rotor blade3531486UNINA