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Panel method for mixed configurations with finite thickness and zero thickness

机译:有限厚度和零厚度的混合配置的面板方法

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摘要

Panel methods are well-known methods for solving potential fluid flow problems. However, mixed configurations of obstacles with finite thickness and zero thickness have not been solved with these methods. Such configurations arise naturally in delta wings, sailing boats, and even in complete aircraft aerodynamics. In this work, a new numerical approach is proposed for solving 2D mixed configurations of obstacles with finite thickness and zero thickness. The method is based on the Dirichlet and Neumann formulations and is checked by comparison with analytical results.
机译:面板法是解决潜在流体流动问题的众所周知的方法。但是,这些方法尚未解决厚度有限和厚度为零的障碍物的混合配置。这种配置自然会出现在三角翼,帆船中,甚至出现在完整的飞机空气动力学中。在这项工作中,提出了一种新的数值方法来求解具有有限厚度和零厚度的障碍物的二维混合构造。该方法基于Dirichlet和Neumann公式,并与分析结果进行了比较。

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