A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.
Name
24013424-MIT.pdf
Description
Full printable version
Size
5 MB
Format
Adobe PDF
Checksum (MD5)
b4267fc7cb26a1155261b428033905c6
Author(s)
Shaw, John, Jr
Advisor(s)
Rene H. Miller.
Date Issued
1967
Publisher
Massachusetts Institute of Technology
Description
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S.
Microfiche copy available in Barker.
Bibliography: leaves 95-96.
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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