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Large Eddy Simulations of a spatially developing incompressible 3D mixing layer using the v-ω formulation

机译:使用v-ω公式的空间发展不可压缩3D混合层的大涡模拟

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摘要

The LES of a 3D mixing layer spatially developing downstream of a flat plate has been conducted for a high Reynolds number (Re{sub}θ = 28.35). To overcome the problem of the pressure condition on the free boundaries, use of the (v-ω) formulation of the Navier-Stokes equations has been preferred over the primitive (v-p) formulation. To deal with the difficult problem of the divergence free constraint on both the velocity and the vorticity field, a new and efficient numerical algorithm has been devised which turns out to be very attractive. The velocity components are computed as a solution of a Cauchy-Riemann problem using a fractional step method. As one of the main advantages of the vorticity-based formulation is the treatment of the free flow boundary conditions, special care has been devoted to these boundary conditions. An optimum approximation of the outflow boundary condition has been carried out which satisfies the conservation of mass, making the long time integration easier and more accurate. The numerical results are compared to a reference experiment [Appl. Sci. Res. 53 (1994) 263; J. Delville, PhD thesis, University of Poitiers, 1995] for a rather high Reynolds number. Using inlet perturbations and the mixed scale model, the LES results agree very well with the reference experiments. The validation of the numerical procedure is reviewed on the mean and fluctuating quantities. Good prediction of the spatial evolution is demonstrated for the distribution of the vorticity thickness as well as for the Reynolds stress profiles and spatial correlations. In order to estimate the quality of the spatio-temporal development, a spectral analysis is also reported on the space and time spectra, pointing out a highly 3D arrangement with length scales and frequencies in rather good agreement with the ones generally admitted.
机译:对于高雷诺数(Reθ= 28.35)已经进行了在空间上在平板下游发展的3D混合层的LES。为了克服自由边界上压力条件的问题,相对于原始(v-p)公式,优选使用Navier-Stokes方程的(v-ω)公式。为了解决速度和涡度场上无散度约束的难题,设计了一种新的高效数值算法,结果证明它非常有吸引力。使用分数步法将速度分量计算为Cauchy-Riemann问题的解。由于基于涡度的公式化的主要优点之一是自由流动边界条件的处理,因此对这些边界条件进行了特别注意。已经进行了流出边界条件的最佳近似,该近似近似满足质量守恒,使得长时间积分更容易且更准确。将数值结果与参考实验进行比较[Appl。科学Res。 53(1994)263; J. Delville,博士学位论文,普瓦捷大学,1995年]得出了相当高的雷诺数。使用入口扰动和混合比例模型,LES结果与参考实验非常吻合。数值程序的验证将在均值和波动量上进行回顾。对于涡旋厚度的分布以及雷诺应力分布和空间相关性,已经证明了对空间演化的良好预测。为了估计时空发展的质量,还对时空频谱进行了频谱分析,指出了高度3D排列,其长度比例和频率与通常认可的高度比例和频率相当吻合。

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