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Higher harmonic blade pitch control : a system for helicopter vibration reduction

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Higher harmonic blade pitch control : a system for helicopter vibration reduction

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Author: Shaw, John
Other Contributors: Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Advisor: Norman D. Ham...et al.
Department: Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Publisher: Massachusetts Institute of Technology
Date Issued: 1980
Description:
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1980.MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.Vita.Includes bibliographical references.
URI: http://hdl.handle.net/1721.1/15817
Keywords: Aeronautics and Astronautics., Pitching (Aerodynamics), Rotors (Helicopters), Blades, Vibration (Aeronautics) Damping

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