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Physics-Based Mesh Fitting Algorithms for Hypersonic Flows Simulations

机译:基于物理的超音速流模拟网格拟合算法

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The computational modeling of high-speed flows is characterized by a plethora of complex physical phenomena that do not appear in lower Mach regimes. The analysis of those flows requires accurate, robust and advanced numerical techniques to capture all flow features properly. The numerical investigation of such flow problems may require extremely fine meshes over narrow regions of the physical domain to resolve the large solution variations. The high-gradient regions are not known to the analyst a-priori. Thus, a-posteriori adaptive techniques are desirable to better capture the relevant flow features. Adaptive mesh algorithms represent a robust procedure improving the quality of the physical results, due to a local increase of the grid resolution at the price of an increased algorithmic complexity. The physics-based r-refinement, implemented within the COOLFluiD platform, consists in repositioning the mesh points according to a flow field variable, while keeping their number and connectivity frozen. The developed mesh refinement algorithms are based on spring networks mainly derivatives of linear spring analogy, the semi torsional spring analogy and the ortho-semi torsional spring analogy based on local physical and geometrical properties depending on a monitored variable. In the present paper, a concise overview of the mesh fitting techniques will be given, followed by some promising results of the physics-based r-refinement.
机译:高速流动的计算建模的特征在于血于络合物物理现象,其不会以较低的马赫制度出现。对这些流程的分析需要准确,强大,先进的数值技术来正确捕获所有流量功能。这种流动问题的数值研究可能需要在物理域的窄区域上极细网格来解决大的解决方案变化。分析师A-priori不知道高梯度区域。因此,希望更好地捕获相关的流动特征。自适应网格算法代表了一种强大的过程,提高了物理结果的质量,这是由于网格分辨率以增加的算法复杂性的价格增加。在CoolFluID平台内实现的物理基R细化包括根据流场变量重新定位网格点,同时保持其数量和连接冻结。开发的网格细化算法基于弹簧网络,主要是线性弹簧类比的衍生物,基于本地物理和几何特性的基于局部物理和几何特性,根据受监控变量,基于局部物理和几何特性的衍生物。在本文中,将给出一种关于网格拟合技术的简明概述,其次是一些基于物理的R细化的有希望的结果。

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