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  5. Secondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascades

Secondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascades

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Author(s)
Renaud, Earl William
Advisor(s)
C.S. Tan.
Date Issued
1991
Publisher
Massachusetts Institute of Technology
Description
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.
Includes bibliographical references (leaves 166-170).
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/1721.1/43059
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