An assessment of computational procedures for eleven-stage compressor response to inlet distortion
Name
54070371-MIT.pdf
Description
Full printable version
Size
2.9 MB
Format
Adobe PDF
Checksum (MD5)
c4d3e9ead461b154057e10a795745030
Author(s)
Chan, Keen Ian, 1972-
Advisor(s)
Yifang Gong and Choon S. Tan.
Date Issued
2003
Publisher
Massachusetts Institute of Technology
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.
Includes bibliographical references (p. 74-76).
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
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