Stagger angle effects on impingement cooling of a rotating turbine blade

Author(s)
Preiser, Uriel Z
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Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Advisor
Alan Harry Epstein.
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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
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Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.
 
MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.
 
Includes bibliographical references.
 
Date issued
1984
URI
http://hdl.handle.net/1721.1/15593
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics.
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