| dc.contributor.advisor |
C.S. Tan. |
en_US |
| dc.contributor.author |
Renaud, Earl William |
en_US |
| dc.date.accessioned |
2008-11-07T18:57:29Z |
|
| dc.date.available |
2008-11-07T18:57:29Z |
|
| dc.date.copyright |
1991 |
en_US |
| dc.date.issued |
1991 |
en_US |
| dc.identifier.uri |
http://hdl.handle.net/1721.1/43059 |
|
| dc.description |
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. |
en_US |
| dc.description |
Includes bibliographical references (leaves 166-170). |
en_US |
| dc.description.statementofresponsibility |
by Earl William Renaud. |
en_US |
| dc.format.extent |
xiv, 170 leaves |
en_US |
| dc.language.iso |
eng |
en_US |
| dc.publisher |
Massachusetts Institute of Technology |
en_US |
| 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. |
en_US |
| dc.rights.uri |
http://dspace.mit.edu/handle/1721.1/7582 |
en_US |
| dc.subject |
Aeronautics and Astronautics |
en_US |
| dc.title |
Secondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascades |
en_US |
| dc.type |
Thesis |
en_US |
| dc.description.degree |
Ph.D. |
en_US |
| dc.contributor.department |
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics |
en_US |
| dc.identifier.oclc |
24400925 |
en_US |
