首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS
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COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS

机译:气动拓扑学变化的拓扑网格上的可压缩流体方程

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The analysis of unsteady fluid flows on moving domains is a very complex task, that may be often tackled using domain remeshing techniques. In the present paper a novel mesh movement strategy is presented. It is based on the blending of simple local edge-swapping with mesh deformation by means of the elastic analogy. To deal with mesh topology changes an extension of the classical Arbitary Lagrangian-Eulerian formulation of the fluid flow equations is developed. In this way the use of interpolations of fluid fields between old and new grid is avoided. Furthermore, this extension allows the easy implementation of high order time integration schemes. Preliminary two dimensional numerical simulations are presented to demonstrate the correctness of the present approach. They shows how this approach guarantees a high quality of the grid without resorting to remeshing, resulting in a very efficient solver useful for the analysis of Fluid-Structure Interaction problems, even for the cases which requires large mesh deformations or changes in the domain topology.
机译:分析运动域上的非稳态流体流动是一项非常复杂的任务,通常可以使用域重新划分技术来解决。在本文中,提出了一种新颖的网格运动策略。它基于通过弹性类比将简单的局部边交换与网格变形混合的基础。为了应对网格拓扑变化,开发了流体流动方程的经典任意拉格朗日-欧拉公式的扩展。这样,避免了在新旧网格之间使用流场插值。此外,此扩展允许轻松实现高阶时间积分方案。初步的二维数值模拟被提出来证明本方法的正确性。他们展示了这种方法如何在不求助于网格重塑的情况下保证了网格的高质量,从而产生了一种非常有效的求解器,可用于分析流固耦合问题,即使对于需要大网格变形或域拓扑变化的情况也是如此。

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