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Simulation of wind turbine wakes on locally refined Cartesian grids

机译:在局部精制的笛卡尔网格上模拟风轮机尾流

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Performing high-fidelity numerical simulations of turbulent flow in multi-turbine wind farms remains a challenging issue mainly because of the large computational resources required to accurately simulate the large disparity of spatial scales. To address this challenge we develop herein a new Adaptive Mesh Refinement (AMR) flow solver to enhance the resolution and improve the efficiency of the Virtual Wind Simulator (VWiS) code,1 which is capable of simulating multi-turbine wind farms in complex terrain. We extend the Curvilinear Immersed Boundary (CURVIB) approach incorporated in the VWiS code to unstructured Cartesian grids with strong coupling between multiple levels of refinement. The challenging issues of flux mismatching or pressure discontinuity across fine/coarse interfaces are overcome by the resulting fully unstructured approach. The efficiency and accuracy of the solver is demonstrated by solving the Navier-Stokes equations in driven cavity flows. Large-eddy simulation (LES) of turbulent flows past a stand alone wind turbine, which is modelled by using the Actuator Line Model (ALM), reveal that computed results obtained in locally refined domains are in good agreement with the experimental measurements. These simulations also show the ability of our method to simulate the rich dynamics on the wake of the turbine.
机译:在多涡轮风电场中对湍流进行高保真数值模拟仍然是一个具有挑战性的问题,这主要是因为需要大量的计算资源来准确地模拟较大的空间尺度差异。为了解决这一挑战,我们在此开发了一种新的自适应网格细化(AMR)流量求解器,以提高分辨率和提高虚拟风力模拟器(VWiS)代码的效率,1可以模拟复杂地形中的多涡轮风电场。我们将合并在VWiS代码中的曲线浸入边界(CURVIB)方法扩展到非结构化的笛卡尔网格,并在多个细化级别之间建立了强耦合。通过最终完全非结构化的方法,可以克服通量不匹配或精细/粗糙界面上的压力不连续性这一具有挑战性的问题。通过求解从动腔流中的Navier-Stokes方程,证明了求解器的效率和准确性。流过独立风力涡轮机的湍流的大涡流模拟(LES),通过使用执行器线模型(ALM)进行建模,揭示了在局部精炼域中获得的计算结果与实验测量值非常吻合。这些模拟还显示了我们的方法能够模拟涡轮机尾流时丰富的动力的能力。

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