A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.

A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S. === Microfiche copy available in Barker. === Bibliography: leaves 95-96. === M.S.

Bibliographic Details
Main Author: Shaw, John, Jr
Other Authors: Rene H. Miller.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2014
Subjects:
Aeronautics and Astronautics
Online Access:http://hdl.handle.net/1721.1/86252

Internet

http://hdl.handle.net/1721.1/86252

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