Finite element analysis (FEA) modeling on adhesive joint for composite fuselage model
In this paper, a finite element modeling via ABAQUS/Explicit simulation on a novel fabrication miniature composite fuselage structure is presented. The fuselage structure is modeled as a continuum composite layup that consisted of a woven C-glass fiber/epoxy 200 g/m 2 composite laminated [90 8] with...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Academic Journals
2011
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| Online Access: | http://psasir.upm.edu.my/id/eprint/23085/ http://psasir.upm.edu.my/id/eprint/23085/ http://psasir.upm.edu.my/id/eprint/23085/1/Finite%20element%20analysis%20%28FEA%29%20modeling%20on%20adhesive%20joint%20for%20composite%20fuselage%20model.pdf |