The effect of ribbon rotor geometry on blade response and stability.
Name
26024871-MIT.pdf
Description
Full printable version
Size
2.76 MB
Format
Adobe PDF
Checksum (MD5)
748cf222d16de234d15bbd5d7b74cb7e
Author(s)
Roeseler, William Gene
Advisor(s)
Norman D. Ham.
Date Issued
1966
Publisher
Massachusetts Institute of Technology
Description
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.
Bibliography: leaf 35.
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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