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Eulerian Method for Ice Crystal Icing with Application to Particle Trajectories and Accretion on a Three-Element Airfoil

机译:冰晶掺杂的欧拉曲面涂布术中的粒子轨迹和三元翼型中的吸积

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The aim of this study is to show the application of an Eulerian method for ice crystal icing to a three-element airfoil in high-lift configuration. The ice crystals have been modeled as non-spherical particles which are subject to convection and/or phase change along their trajectories. On impact with the airfoil surface the ice crystals will either stick to the surface or rebound from the airfoil unchanged or as a number of fragments. The evolution of the secondary cloud containing these rebounded or shattered fragments is computed as well. It is concluded that an Eulerian method is a convenient method to compute trajectories of (melting) ice crystals for a high-lift configuration such as a three-element airfoil if certain limitations with regard to the secondary cloud of particles are taken into account.
机译:本研究的目的是展示欧拉法在高升力配置中涂上冰晶晶体的应用方法。冰晶已经被建模为非球形颗粒,其沿着它们的轨迹进行对流和/或相变。在翼型表面的冲击上,冰晶将粘附到表面上或从翼型中的反弹不变或作为许多碎片。还计算含有这些反弹或破碎的片段的次云的演变。得出结论,欧拉方法是一种方便的方法来计算用于高升力构造的(熔化)冰晶的轨迹,例如三元翼型,如果考虑到颗粒的次级云的某些限制,则是三元件翼型。

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