Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment
Name
51276747-MIT.pdf
Description
Full printable version
Size
9.51 MB
Format
Adobe PDF
Checksum (MD5)
6ecc2fe1c1f291681c6f9c706401d2c3
Author(s)
Lenglin, Geoffroy (Geoffroy Philippe), 1976-
Advisor(s)
Choon S. Tan.
Date Issued
2002
Publisher
Massachusetts Institute of Technology
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.
Includes bibliographical references (p. 90-91).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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copyright. They may be viewed from this source for any purpose, but
reproduction or distribution in any format is prohibited without written
permission. See provided URL for inquiries about permission.
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