Structural design improvement of unmanned aerial vehicle wing
Almost all engineering systems experience strength versus weight conflict of some description. In the case of airplane wing, there are two primary requirements which must be considered during the structural design process: high strength and stiffness, and lower weight. Due to the restricted nature o...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 語言: | English |
| 出版: |
2014
|
| 主題: | |
| 在線閱讀: | http://eprints.utm.my/id/eprint/53465/25/GunasegaranKanesanMFKM2014.pdf |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
成為第一個發表評論!