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.

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

Similar Items

Similar Items