Cover Image

Rotating shake test and modal analysis of a model helicopter rotor blade /

Bibliographic Details
Main Authors: Wilkie, W. Keats (Author), Mirick, Paul H. (Author), Langston, Chester W. (Author)
Corporate Authors: Vehicle Technology Center (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, June 1997.
Series:NASA technical memorandum ; 4760.
Subjects:
Rotary wings.
Helicopters.
Aeroelasticity.
Hovering.
Torsion.
Online Access:https://purl.fdlp.gov/GPO/gpo65480
Description
Item Description:Title 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."
Physical Description:1 online resource (15 pages.) : illustrations.
Bibliography:Includes bibliographical references (page 15).