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  5. Blade passage flow structure effects on axial compressor rotating stall inception

Blade passage flow structure effects on axial compressor rotating stall inception

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Author(s)
Hoying, Donald Andrew
Advisor(s)
Edward M. Greitzer.
Date Issued
1996
Publisher
Massachusetts Institute of Technology
Description
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.
Includes bibliographical references (p. 125-130).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
M.I.T. theses are protected by 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.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/10623
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