dc.contributor.advisor | James W. Mar. | en_US |
dc.contributor.author | Nolet, Stephen C | en_US |
dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
dc.date.accessioned | 2010-01-07T20:21:18Z | |
dc.date.available | 2010-01-07T20:21:18Z | |
dc.date.copyright | 1984 | en_US |
dc.date.issued | 1984 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/50277 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984. | en_US |
dc.description | Microfiche copy available in Archives and Barker. | en_US |
dc.description | Includes bibliographical references. | en_US |
dc.description.statementofresponsibility | by Stephen C. Nolet. | en_US |
dc.format.extent | 181 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 | The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading | 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 | 12264853 | en_US |