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Numerical Simulation of Ice Accretions Based on Unstructured Grids

机译:基于非结构化网格的积冰数值模拟

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An Eulerian method to numerically simulate ice accretions on airfoils based on unstructured grids has been presented. The Euler Equations are employed to solve the flowfields of the airfoils. The governing equations for droplets are solved based on the velocity distribution of the airflow to obtain the collection efficiency on the airfoil surfaces. The different freezing models are employed to simulate the freezing processes of the rime and glaze ice in order to calculate the ice amount. The ice accretions on a NACA 0012 airfoil have been simulated and the comparison with the experimental data indicates that the simulated method presented is feasible and effective.
机译:提出了一种基于非结构化网格的数值模拟机翼上结冰的欧拉方法。欧拉方程用于求解机翼的流场。基于气流的速度分布求解液滴的控制方程,以获得在翼型表面上的收集效率。为了计算冰量,采用了不同的冷冻模型来模拟霜和釉冰的冷冻过程。对NACA 0012机翼上的积冰进行了模拟,并与实验数据进行了比较,表明所提出的模拟方法是可行和有效的。

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