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Large-Eddy Simulation of Compressible Flows with an Analytic Non-Equilibrium Wall Model

机译:解析非平衡壁模型对可压缩流的大涡模拟

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An analytic wall model suitable for flows in the presence of equilibrium or non-equilbrium effects is derived. The model is predicated upon definition of a new velocity scale that encompasses both viscous and pressure gradient effects, thereby providing a unified approach to simulating separated and attached flows. Asymptotic solutions of the surface layer flow are derived considering the effects of both pressure gradients and convective terms in the streamwise momentum equation resulting in a wall model consistent with flow physics. Within the context of a two-dimensional shock boundary layer interaction at low Reynolds number, the model captures the relevant features, both in the time-mean and unsteady sense. It is demonstrated that inclusion of convective terms in the analytic wall model results in the most accurate representation of the interaction region whereas it over-predicts the wall-shear-stress in equilbrium and near-equilibrium regions. In contrast, considering only pressure-gradient effects in the analytic wall model results in predictions of wall shear stress of increasing accuracy with increasing wall-model/large-eddy-simulation interface distance in all regions of the flow. While the low-Reynolds number simulations were conducted to have a reference wall-resolved simulation, the equilibrium turbulent boundary layer upstream of the interaction displayed a noticeable log-layer region, justifying the separation-of-scales assumption adopted in the wall modeling approach.
机译:推导了适用于存在平衡或非平衡效应的流动的分析墙模型。该模型基于包含粘性和压力梯度效应的新速度标度的定义,从而提供了一种模拟分离和附加流动的统一方法。考虑到流向动量方程中的压力梯度和对流项的影响,得出了表面层流的渐近解,从而得出了与流动物理一致的壁模型。在低雷诺数的二维激波边界层相互作用的背景下,该模型捕获了均值和非稳态的相关特征。结果表明,将对流项包含在解析壁模型中可以最准确地表示相互作用区域,而过分预测了平衡和近平衡区域中的壁切应力。相比之下,仅考虑分析壁模型中的压力梯度效应,就可以预测壁切应力随着流的所有区域中壁模型/大涡流模拟界面距离的增加而提高的准确性。虽然进行了低雷诺数模拟以得到参考壁解析模拟,但相互作用上游的平衡湍流边界层显示了显着的对数层区域,这证明了在壁建模方法中采用的比例分离假设是合理的。

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