Crush simulation of woven c-glass/epoxy unmanned ariel vehicle fuselage section
A quasi-static crush analysis of an unmanned aerial vehicle (UAV) fuselage section made of woven c-glass/epoxy has been conducted using the finite element simulation via ABAQUS. The main material and strength properties of the c-glass/epoxy (200 g/m2) which were needed in the ABAQUS analyses were ob...
| Main Authors: | , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Department of Mechanical Engineering, University of Malaya
2010
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| Online Access: | http://psasir.upm.edu.my/id/eprint/13833/1/Crush%20simulation%20of%20woven%20c-glassepoxy%20unmanned%20ariel%20vehicle%20fuselage%20section.pdf |