| dc.contributor.advisor | Robert C. Seamans, Jr. | en_US |
| dc.contributor.author | Bakemeyer, William F | en_US |
| dc.contributor.author | Enders, William H | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Aeronautical Engineering Department. | |
| dc.date.accessioned | 2005-08-05T16:06:01Z | |
| dc.date.available | 2005-08-05T16:06:01Z | |
| dc.date.issued | 1951 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/15548 | |
| dc.description | Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1951. | en_US |
| dc.description | Bibliography: leaves 72-73. | en_US |
| dc.description.statementofresponsibility | by William F. Bakemeyer and William H. Enders. | en_US |
| dc.format.extent | vii, 77 leaves | en_US |
| dc.format.extent | 6155949 bytes | |
| dc.format.extent | 6155705 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 | Aeronautical Engineering Dept. | en_US |
| dc.title | Design of a normal acceleration limiting system for a high-performance aircraft | 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 | 11535317 | en_US |
