Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads
By: Matthew L. Wilbur ... [et al.].
Contributors: Wilbur, Matthew L.; Langley Research Center.; U.S. Army Research Laboratory.
Series: ARL-TR -- 1401; NASA/TM -- 1998-206281; NASA technical memorandum -- 1998-206281.; Army Research Laboratory technical report -- ALR-TR-1401.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from the National Technical Information Service
Published: 1998
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Number of pages: 246
Subjects: Helicopters -- Vibration.; Structural dynamics.
Notes: "January 1998."

"Performing organization report number L-17353"--Report documentation page.

Includes bibliographical references (p. 5).

Performed by Vehicle Technology Center, U.S. Army Research Laboratory and Langley Research Center for the National Aeronautics and Space Administration WU 505-63-36-02