| dc.contributor.advisor | Norman D. Ham. | en_US |
| dc.contributor.author | Roeseler, William Gene | en_US |
| dc.date.accessioned | 2007-08-29T20:48:39Z | |
| dc.date.available | 2007-08-29T20:48:39Z | |
| dc.date.issued | 1966 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/38720 | |
| dc.description | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S. | en_US |
| dc.description | Bibliography: leaf 35. | en_US |
| dc.format.extent | [8], 35 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 effect of ribbon rotor geometry on blade response and stability. | 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 | 26024871 | en_US |
