The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.
| Main Author: | |
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| Other Authors: | |
| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2007
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| Online Access: | http://hdl.handle.net/1721.1/39013 |
| _version_ | 1811070269505142784 |
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| author | D'Angelo, Michael R. (Michael Ronald) |
| author2 | Eugene E. Covert. |
| author_facet | Eugene E. Covert. D'Angelo, Michael R. (Michael Ronald) |
| author_sort | D'Angelo, Michael R. (Michael Ronald) |
| collection | MIT |
| description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. |
| first_indexed | 2024-09-23T08:33:48Z |
| format | Thesis |
| id | mit-1721.1/39013 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T08:33:48Z |
| publishDate | 2007 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/390132019-04-09T18:29:38Z The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method D'Angelo, Michael R. (Michael Ronald) Eugene E. Covert. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. Includes bibliographical references (leaves 86-88). by Michael R. D'Angelo. M.S. 2007-09-28T13:33:24Z 2007-09-28T13:33:24Z 1988 1989 Thesis http://hdl.handle.net/1721.1/39013 20404644 eng 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. http://dspace.mit.edu/handle/1721.1/7582 121 leaves application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics. D'Angelo, Michael R. (Michael Ronald) The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method |
| title | The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method |
| title_full | The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method |
| title_fullStr | The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method |
| title_full_unstemmed | The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method |
| title_short | The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method |
| title_sort | effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid inviscid vortex panel method |
| topic | Aeronautics and Astronautics. |
| url | http://hdl.handle.net/1721.1/39013 |
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