Finite element analysis of cohesive element for glass epoxy composite fuselage model
In this research, a numerical simulation on a newly introduced fabrication miniature composite fuselage structure - a glass epoxy composite laminated with adhesively bonded butt joint under axial compression loading is presented. A FEA via ABAQUS/Explicit is utilized to capture the complete compress...
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| 格式: | Thesis |
| 语言: | 英语 |
| 出版: |
2011
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| 在线阅读: | http://psasir.upm.edu.my/id/eprint/41770/1/FK%202011%202R.pdf |