dc.contributor.advisor | Choon S. Tan. | en_US |
dc.contributor.author | Stanislaw, Gregory Scott | en_US |
dc.date.accessioned | 2009-12-10T18:54:21Z | |
dc.date.available | 2009-12-10T18:54:21Z | |
dc.date.copyright | 1997 | en_US |
dc.date.issued | 1997 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/49969 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997. | en_US |
dc.description | Includes bibliographical references (p. 78-80). | en_US |
dc.description.statementofresponsibility | by Gregory Scott Stanislaw. | en_US |
dc.format.extent | 102 p. | 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 | Utility of the flow substitution principle for high speed propulsion applications | en_US |
dc.type | Thesis | en_US |
dc.description.degree | M.S. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 36829827 | en_US |