Effects of leading-edge tubercles on wing flutter speeds
The dynamic aeroelastic effects on wings modified with bio-inspired leading-edge (LE) tubercles are examined in this study. We adopt a state-space aeroelastic model via the coupling of unsteady vortex-lattice method and a composite beam to evaluate stability margins as a result of LE tubercles on a...
Saved in:
Main Authors: | , , |
---|---|
其他作者: | |
格式: | Article |
語言: | English |
出版: |
2016
|
主題: | |
在線閱讀: | https://hdl.handle.net/10356/80338 http://hdl.handle.net/10220/40684 |
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 |
成為第一個發表評論!