| dc.contributor.advisor | H.H. Pian. | en_US |
| dc.contributor.author | Li, Ming-Sang | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2008-02-04T20:51:07Z | |
| dc.date.available | 2008-02-04T20:51:07Z | |
| dc.date.copyright | 1989 | en_US |
| dc.date.issued | 1989 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/40145 | |
| dc.description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. | en_US |
| dc.description | Includes bibliographical references (leaves 259-272). | en_US |
| dc.description.statementofresponsibility | by Ming-Sang Li. | en_US |
| dc.format.extent | 279 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 | Higher order laminated composite plate analysis by hybrid finite element method | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | Ph.D. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 22248778 | en_US |
