Influence of Reynolds number and blade geometry on low pressure turbine performance
Name
37896579-MIT.pdf
Description
Full printable version
Size
25.82 MB
Format
Adobe PDF
Checksum (MD5)
02e9fb19fee4aeffd86e5b870ddd0f7d
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
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.
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.
Persistent DSpace Link