摘要
The closure parameters introduced in transition models can compromise the accuracy of prediction results. This paper investigated the uncertainty caused by the closure parameters in transition models (γ and k-ω-γ), and identified the key parameters that have the greatest impact on quantities of interest. The uncertainty was propagated by the point-collocation no-intrusive polynomial chaos method, and the relative contribution of each parameter to uncertainty was assessed by the Sobol index. The natural transition flow (Schubauer-Klebanoff flat plate) and low-velocity airfoil flow (NLF0416 airfoil) were chosen for computational cases. The results, which are highly dependent on the closure parameters, validate the necessity of uncertainty research. The parameters of the k-ω-γ model are more sensitive than those of the γ model. In the γ model, the most critical parameter is CTU2, which is negatively related to the transition position, i.e., the transition delays when CTU2 increases and advances when CTU2 decreases. In the k-ω-γ model, the most critical parameter is C2, which is positively related to the transition position.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 04022105-1 |
| 期刊 | Journal of Aerospace Engineering |
| 卷 | 36 |
| 期 | 1 |
| DOI | |
| 出版状态 | 已出版 - 1 1月 2023 |
指纹
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