Numerical Investigation on Flow Separation Control of Low Reynolds Number Sinusoidal Aerofoils
The paper presents a computational analysis of the characteristics of a NACA 634-021 aerofoil incorporated with sinusoidal leading-edge protuberances at Re = 14,000. The protuberances are characterized by an amplitude and wavelength of 12% and 50% of the aerofoil chord length respectively. An unstea...
Saved in:
| Main Authors: | , , |
|---|---|
| 其他作者: | |
| 格式: | Conference or Workshop Item |
| 語言: | English |
| 出版: |
2017
|
| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/83344 http://hdl.handle.net/10220/42539 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|