Stagger angle effects on impingement cooling of a rotating turbine blade
Name
11905608-MIT.pdf
Description
Full printable version
Size
8.11 MB
Format
Adobe PDF
Checksum (MD5)
c335b581e7b8165335bc762a17346b17
Author(s)
Preiser, Uriel Z
Advisor(s)
Alan Harry Epstein.
Date Issued
1984
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.
MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.
Includes bibliographical references.
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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.
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