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

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997. / Includes bibliographical references (p. 172-173). / by Mark Eric Bury. / M.S.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/50310
Date January 1997
CreatorsBury, Mark Eric
ContributorsChoon S. Tan., Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Format173 p., application/pdf
RightsM.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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