摘要
Wall pressure distribution induced by the saw-tooth flap has been investigated with electronic pressure scanner in wind tunnel. The results show that the shear layer of the saw-tooth flap separates at x/h=-6 up-stream and reattached at x/h=20 downstream, which is the same with the plate flap; the transverse location of the flap has little influence on the mean pressure distribution, and the distribution of pressure fluctuation along the saw-tooth groove is greater than that along the saw-tooth tip; the saw-tooth can block the flow and much more effectively reduce the pressure fluctuation downstream.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 424-427 |
| 页数 | 4 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 28 |
| 期 | 4 |
| 出版状态 | 已出版 - 8月 2002 |
指纹
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