Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 578-581 |
| Number of pages | 4 |
| Journal | Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica |
| Volume | 27 |
| Issue number | 5 |
| State | Published - Oct 2009 |
Keywords
- CFD method
- Infinite swept wing
- Wind tunnel testing
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