摘要
In order to achieve the fluid field of an "Infinite Swept Wing" in a wind tunnel, wall-liners formed from the inviscid streamlines of an infinite swept wing are designed to correct the side wall influence of the wind tunnel. According to CFD results, in a relatively large range in span direction, the flow around the wind tunnel test model is nearly the same as the flow around an infinite swept wing, even with a small aspect ratio.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 578-581 |
| 页数 | 4 |
| 期刊 | Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica |
| 卷 | 27 |
| 期 | 5 |
| 出版状态 | 已出版 - 10月 2009 |