Aerodynamics investigation of MAV with flexible wing
This report describes research performed on various configurations of a flexible-wing Micro Air Vehicle (MAV). Flexible-wing MAV’s advantage over rigid-wing MAV is that it is able to fly much smoother in gusty wind conditions. As such, wind tunnel experiments at free stream velocity of 21 m/s were c...
Saved in:
| 主要作者: | |
|---|---|
| 其他作者: | |
| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2011
|
| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/44674 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
| 機構: | Nanyang Technological University |
| 語言: | English |