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Numerical Simulation of Ice Accretions Based on Unstructured Grids

机译:基于非结构化网格的冰渐凝的数值模拟

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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:已经介绍了基于非结构化网格的数值模拟翼型上的冰空间的欧拉方法。使用欧拉方程来解决翼型的流动场。基于气流的速度分布来解决液滴的控制方程,以获得翼型表面上的收集效率。采用不同的冷冻模型来模拟铃声和釉冰的冷冻过程,以计算冰量。已经模拟了NaCA 0012翼型的冰吸收,并且与实验数据的比较表明所呈现的模拟方法是可行和有效的。

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