The effect of ribbon rotor geometry on blade response and stability.
Author(s)
Roeseler, William Gene![Thumbnail](/bitstream/handle/1721.1/38720/26024871-MIT.pdf.jpg?sequence=5&isAllowed=y)
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Advisor
Norman D. Ham.
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Metadata
Show full item recordDescription
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S. Bibliography: leaf 35.
Date issued
1966Department
Massachusetts Institute of Technology. Department of Aeronautics and AstronauticsPublisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics