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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
Description
Item Description:Title 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."
Physical Description:1 online resource (iv, 58 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 22-24).