A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.
1967
ix, 96 pages
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S.
Microfiche copy available in Barker.
Bibliography: leaves 95-96.
Theses
Electronic Resource
English
Higher harmonic blade pitch control : a system for helicopter vibration reduction
DSpace@MIT | 1980
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