Crash Simulation Of A Composite Unmanned Aerial Vehicle Fuselage
In this research the results of experimental works and numerical simulation works pertaining to the crash behavior and crashworthiness characteristic of the upper part of the composite unmanned aerial vehicle (UAV) fuselage sections that were subjected to quasi-static transverse compressive loading...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 语言: | English English |
| 出版: |
2007
|
| 主题: | |
| 在线阅读: | http://psasir.upm.edu.my/id/eprint/5251/1/FK_2007_47.pdf |
| 标签: |
添加标签
没有标签, 成为第一个标记此记录!
|
成为第一个发表评论!