dc.contributor.advisor | Earll M. Murman, Mårten Landahl. | en_US |
dc.contributor.author | Modiano, David | en_US |
dc.date.accessioned | 2009-12-10T18:44:41Z | |
dc.date.available | 2009-12-10T18:44:41Z | |
dc.date.copyright | 1993 | en_US |
dc.date.issued | 1993 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/49895 | |
dc.description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993. | en_US |
dc.description | Includes bibliographical references (leaves 139-146). | en_US |
dc.description.statementofresponsibility | by David Laurence Modiano. | en_US |
dc.format.extent | 146 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 | Adaptive mesh Euler equation computation of vortex breakdown in delta wing flow | 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 | 28141922 | en_US |