| dc.contributor.advisor | James W. Mar. | en_US |
| dc.contributor.author | Taylor, Matthew Claire | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2008-04-23T14:34:18Z | |
| dc.date.available | 2008-04-23T14:34:18Z | |
| dc.date.copyright | 1989 | en_US |
| dc.date.issued | 1989 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/41237 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. | en_US |
| dc.description | Includes bibliographical references (leaves 135-136). | en_US |
| dc.description.statementofresponsibility | by Matthew Claire Taylor. | en_US |
| dc.format.extent | 202 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 | en_US |
| dc.subject | Aeronautics and Astronautics. | en_US |
| dc.title | Damage tolerance of composite honeycomb sandwich panels under quasi-static bending and cyclic compression | 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 | 20834669 | en_US |
