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...
Saved in:
| Main Authors: | , , , , , |
|---|---|
| 格式: | Article |
| 語言: | English |
| 出版: |
Department of Mechanical Engineering, University of Malaya
2010
|
| 在線閱讀: | http://psasir.upm.edu.my/id/eprint/13833/1/Crush%20simulation%20of%20woven%20c-glassepoxy%20unmanned%20ariel%20vehicle%20fuselage%20section.pdf |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|