A compressible, high frequency numerical model of helicopter noise due to blade/vortex interaction
Name
07991399-MIT.pdf
Size
45.26 MB
Format
Adobe PDF
Checksum (MD5)
34326a23fffda693dea15b69a9713e8d
Author(s)
Lima, Luiz Hamilton de Resende.
Advisor(s)
Sheila Evans Widnall.
Date Issued
1980
Publisher
Massachusetts Institute of Technology
Description
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1980
Includes bibliographical references.
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
MIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.
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