The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.
| Main Author: | |
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| Other Authors: | |
| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2010
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| Online Access: | http://hdl.handle.net/1721.1/50277 |
| _version_ | 1826211545906937856 |
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| author | Nolet, Stephen C |
| author2 | James W. Mar. |
| author_facet | James W. Mar. Nolet, Stephen C |
| author_sort | Nolet, Stephen C |
| collection | MIT |
| description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984. |
| first_indexed | 2024-09-23T15:07:42Z |
| format | Thesis |
| id | mit-1721.1/50277 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T15:07:42Z |
| publishDate | 2010 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/502772019-04-11T11:13:59Z The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading Nolet, Stephen C James W. Mar. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984. Microfiche copy available in Archives and Barker. Includes bibliographical references. by Stephen C. Nolet. M.S. 2010-01-07T20:21:18Z 2010-01-07T20:21:18Z 1984 1984 Thesis http://hdl.handle.net/1721.1/50277 12264853 eng 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. http://dspace.mit.edu/handle/1721.1/7582 181 leaves application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics. Nolet, Stephen C The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading |
| title | The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading |
| title_full | The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading |
| title_fullStr | The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading |
| title_full_unstemmed | The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading |
| title_short | The effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loading |
| title_sort | effect of ply thickness on the initiation and growth of delamination in graphite epoxy laminates with holes under compressive cyclic loading |
| topic | Aeronautics and Astronautics. |
| url | http://hdl.handle.net/1721.1/50277 |
| work_keys_str_mv | AT noletstephenc theeffectofplythicknessontheinitiationandgrowthofdelaminationingraphiteepoxylaminateswithholesundercompressivecyclicloading AT noletstephenc effectofplythicknessontheinitiationandgrowthofdelaminationingraphiteepoxylaminateswithholesundercompressivecyclicloading |