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...
| मुख्य लेखक: | |
|---|---|
| स्वरूप: | थीसिस |
| भाषा: | अंग्रेज़ी |
| प्रकाशित: |
2011
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| विषय: | |
| ऑनलाइन पहुंच: | http://psasir.upm.edu.my/id/eprint/41770/1/FK%202011%202R.pdf |