Parametric study on cohesive element for composite fuselage model
In this paper, a numerical simulation on a new fabrication miniature composite fuselage structure- a woven composite laminated with an adhesively bonded butt joint under the axial compression loading is presented. A FEA via Abaqus/Explicit was utilized to capture the complete compressive responses t...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Trans Tech Publications
2011
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| Online Access: | http://psasir.upm.edu.my/id/eprint/23081/1/Parametric%20study%20on%20cohesive%20element%20for%20composite%20fuselage%20model.pdf |