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...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 語言: | English |
| 出版: |
2011
|
| 在線閱讀: | http://psasir.upm.edu.my/id/eprint/41770/1/FK%202011%202R.pdf http://psasir.upm.edu.my/id/eprint/41770/ |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|