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  5. Effects of compressor face boundary conditions on the dynamic behavior of supersonic inlets

Effects of compressor face boundary conditions on the dynamic behavior of supersonic inlets

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Author(s)
Thammavichai, Jackkrit
Advisor(s)
Choon S. Tan, Edward M. Greitzer.
Date Issued
1996
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.
Includes bibliographical references (p. 69-70).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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permission. See provided URL for inquiries about permission.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/47397
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