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.

Bibliographic Details
Main Author:	Shaw, John, Jr
Other Authors:	Rene H. Miller.
Format:	Thesis
Language:	eng
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