Optimal placement of tuning masses for vibration reduction in helicopter rotor blades
By: Jocelyn I. Pritchard and Howard M. Adelman.
Contributors: Adelman, Howard M.; Langley Research Center.; United States. Army Aviation Research and Technology Activity.
Series: NASA technical memorandum -- 100562.; AVSCOM technical report -- 88-B-003.; AVSCOM technical report -- 88-B-3.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command, Aviation R&T Activity
Published: 1988
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Structural dynamics.; Vibration (Aeronautics)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.