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A New Extension For K-ω Turbulence Models To Account For Wall Roughness

机译:K-ω湍流模型的新扩展以解决壁粗糙度

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This paper presents a new extension for k-ω turbulence models to account for surface roughness for transitionally and fully rough surfaces. It is based on the equivalent sand grain approach and accounts for theoretical considerations on the log-layer solution for fully rough surfaces. An appropriate behaviour for transitional roughness is achieved by means of wall values for k and ω which depend on the roughness Reynolds number. In the limit of vanishing roughness, the smooth wall boundary condition is recovered. For the full range of roughness Reynolds numbers the new roughness modification gives very successful predictions for a variety of flat plate turbulent boundary layer flows and for the pipe flow experiments by Nikuradse. The new method allows for the simulation of flows over rough surfaces at the same grid resolution requirements as for smooth walls. Thereby the extremely fine near-wall mesh resolution required by the Wilcox roughness modification is avoided. Secondly the new roughness modification gives significantly improved predictions in skin friction for transitional roughness Reynolds numbers compared to the roughness extension by Wilcox. Thirdly, the new roughness extension does not require a modification of the SST k-ω model, whereas a modification is necessary if the roughness extension by Wilcox is used. Finally the new method is applied successfully to predict the aerodynamic effects of surface roughness on the flow past an airfoil in highlift conditions.
机译:本文提出了k-ω湍流模型的新扩展,以考虑过渡和完全粗糙表面的表面粗糙度。它基于等效的沙粒方法,并针对完全粗糙表面的对数层解决方案提供了理论考虑。通过依赖于粗糙度雷诺数的k和ω的壁值,可以实现过渡粗糙度的适当性能。在消失的极限内,恢复了光滑的壁边界条件。对于整个粗糙度雷诺数,新的粗糙度修正可以很好地预测各种平板湍流边界层流以及Nikuradse进行的管道流实验。新方法允许以与光滑墙相同的网格分辨率要求模拟粗糙表面上的流动。因此,避免了Wilcox粗糙度修改所要求的极精细的近壁网格分辨率。其次,与Wilcox进行的粗糙度扩展相比,新的粗糙度修改可以显着改善过渡摩擦雷诺数对皮肤摩擦的预测。第三,新的粗糙度扩展不需要修改SSTk-ω模型,而如果使用Wilcox进行粗糙度扩展,则必须进行修改。最终,该新方法成功地应用于预测在高升力条件下表面粗糙度对流经机翼的气流的空气动力学影响。

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