02284nam 2200589I 450 991070723990332120160621153028.0(CKB)5470000002463110(OCoLC)951986585(EXLCZ)99547000000246311020160621j199605 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAn aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation /W. Keats Wilkie, K.C. ParkHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,May 1996.1 online resource (iv, 58 pages)illustrationsNASA technical memorandum ;110252Title from title screen (viewed June 21, 2016)."May 1996.""Performing organization: NASA Langley Research Center, Hampton, VA and Vehicle Structures Directorate, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton,VA"--Report documentation page."ARL-MR-328."Includes bibliographical references (pages 22-24).AeroelasticitynasatHelicoptersnasatFiber compositesnasatRotary wingsnasatUnsteady aerodynamicsnasatDifferential equationsnasatGalerkin methodnasatNumerical integrationnasatAeroelasticity.Helicopters.Fiber composites.Rotary wings.Unsteady aerodynamics.Differential equations.Galerkin method.Numerical integration.Wilkie W. Keats1410623Park K. C.U.S. Army Research Laboratory.Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707239903321An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation3499760UNINA