| dc.contributor.advisor | Eugene E. Covert. | en_US |
| dc.contributor.author | D'Angelo, Michael R. (Michael Ronald) | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2007-09-28T13:33:24Z | |
| dc.date.available | 2007-09-28T13:33:24Z | |
| dc.date.copyright | 1988 | en_US |
| dc.date.issued | 1989 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/39013 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. | en_US |
| dc.description | Includes bibliographical references (leaves 86-88). | en_US |
| dc.description.statementofresponsibility | by Michael R. D'Angelo. | en_US |
| dc.format.extent | 121 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 | |
| dc.subject | Aeronautics and Astronautics. | en_US |
| dc.title | The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method | 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 | 20404644 | en_US |
