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  5. Influence of Reynolds number and blade geometry on low pressure turbine performance

Influence of Reynolds number and blade geometry on low pressure turbine performance

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Author(s)
Bury, Mark Eric
Advisor(s)
Choon S. Tan.
Date Issued
1997
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.
Includes bibliographical references (p. 172-173).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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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/1721.1/50310
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