| dc.contributor.advisor | Judson R. Baron. | en_US |
| dc.contributor.author | Robinson, Donald Edwin | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2007-01-10T15:51:16Z | |
| dc.date.available | 2007-01-10T15:51:16Z | |
| dc.date.copyright | 1988 | en_US |
| dc.date.issued | 1988 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/35342 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988. | en_US |
| dc.description | Includes bibliographical references. | en_US |
| dc.description.statementofresponsibility | by Donald Edwin Robinson. | en_US |
| dc.format.extent | 127 leaves | en_US |
| dc.format.extent | 4311167 bytes | |
| dc.format.extent | 4601618 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 | Implementation of a separated flow panel method for wall effects on finite swept wings | 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 | 20054849 | en_US |
