Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
The flying mechanism is unable to escape from the drag force, especially the drag force generated from the wingtip and trailing edge vortices due to the unbalanced pressure between the upper and lower surface. Then, Richard T. Whitcomb, the scientist at NASA Laboratory introduced the winglet structu...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 语言: | English |
| 出版: |
2023
|
| 主题: | |
| 在线阅读: | https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf |
| 标签: |
添加标签
没有标签, 成为第一个标记此记录!
|