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Massachusetts Institute of Technology
Stagger angle effects on impingement cooling of a rotating turbine blade
Abstract
dc:descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.
Degree
thesis:*- Department dc:contributor.department
- Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
- Grantor dc:publisher
- Massachusetts Institute of Technology
- Year dc:date.issued
- 1984
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Preiser, Uriel Z
- Advisor dc:contributor.advisor
-
- Alan Harry Epstein.
Subjects
dc:subject × 1Rights
dc:rights- Statement dc:rights
-
- 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.
- Licence dc:rights.uri
- Language dc:language.iso
- eng
Identifiers
dc:identifier.*- Handle dc:identifier.uri
- http://hdl.handle.net/1721.1/15593
- OAI identifier oai:identifier
- oai:dspace.mit.edu:1721.1/15593