dc.contributor.advisor | James D. Paduano. | en_US |
dc.contributor.author | Van Schalkwyk, Christiaan Mauritz | en_US |
dc.date.accessioned | 2005-08-18T14:33:44Z | |
dc.date.available | 2005-08-18T14:33:44Z | |
dc.date.copyright | 1996 | en_US |
dc.date.issued | 1996 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/10827 | |
dc.description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996. | en_US |
dc.description | Includes bibliographical references (p. 179-182). | en_US |
dc.description.statementofresponsibility | by Christiaan Mauritz Van Schalkwyk. | en_US |
dc.format.extent | 182 p. | en_US |
dc.format.extent | 8634375 bytes | |
dc.format.extent | 8634129 bytes | |
dc.format.mimetype | application/pdf | |
dc.format.mimetype | application/pdf | |
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 | |
dc.subject | Aeronautics and Astronautics | en_US |
dc.title | Active control rotating stall with inlet distortion | en_US |
dc.type | Thesis | en_US |
dc.description.degree | Ph.D. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 35264031 | en_US |