Computational analysis of double rotating cylinders for conceptual design of an estol, fixed wing UAV
Many efforts in Unmanned Aerial Vehicle (UAV) aerodynamic design technology led to a broad of additional applications. Magnus effect is the effect of moving airstream to the spinning ball or cylinder. Previous studies revealed the feasibility of Magnus effect on rotating cylinder producing lift whic...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 语言: | English |
| 出版: |
2017
|
| 主题: | |
| 在线阅读: | http://psasir.upm.edu.my/id/eprint/76076/1/FK%202018%20156%20-%20IR.pdf |
| 标签: |
添加标签
没有标签, 成为第一个标记此记录!
|