摘要
Section 1 of the full paper explains our prediction method mentioned in the title, which we believe is effective and whose core is: using two-dimensional Reynolds-averaged Navier-Stokes equations, we calculate the flow around a conventional sharp trailing edge airfoil and its flatback version employing γ-Rẽ θt transition prediction method based on SST turbulence model; the aerodynamic noise of the flatback airfoil is then computed using hybrid method combining the former CFD results with the Ffowcs Williams-Hawkings(FW-H) equation. Section 2 presents both aerodynamic and acoustic results in Figs. 3 through 9, and analyze most of them, showing preliminarily that the calculated results are in good agreement with experimental data; thus section 2 indicates that our method is successful for predicting aerodynamic noise for wind turbine flatback airfoils.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 513-517 |
| 页数 | 5 |
| 期刊 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| 卷 | 30 |
| 期 | 4 |
| 出版状态 | 已出版 - 8月 2012 |
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