An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation /

Bibliographic Details

Main Authors:	Wilkie, W. Keats (Author), Park, K. C. (Author)
Corporate Authors:	U.S. Army Research Laboratory, United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1996.
Series:	NASA technical memorandum ; 110252.
Subjects:	Aeroelasticity. Helicopters. Fiber composites. Rotary wings. Unsteady aerodynamics. Differential equations. Galerkin method. Numerical integration.
Online Access:	https://purl.fdlp.gov/GPO/gpo67751