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A generalized framework for high order anisotropic mesh adaptation

机译:高阶各向异性网格自适应的通用框架

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摘要

We present a method for anisotropically adapting meshes for high order (p > 2) finite volume methods. We accomplish this by assuming a polynomial error measure based on the local reconstruction. We then use Fourier series to choose a metric function that approximates our error measure. This approach is theoretically valid for any solution order, with any number of variables and any number of dimensions. Using both second and third order solvers, we present examples of two-dimensional subsonic viscous and inviscid flow around the NACA-0012 airfoil. These test cases demonstrate that mesh refinement based on our metric converges to an accurate solution much faster than with uniform refinement. For subsonic viscous flows, we also show that anisotropic refinement is more efficient than isotropic refinement. By limiting the magnitude of our error measure for a transonic inviscid flow, we demonstrate that our metric can be effective even in the presence of discontinuities. We also examined using second derivatives to estimate the error for third order solutions. While this is less theoretically sound, we found little difference in the resulting accuracy.
机译:我们提出了一种各向异性适应高阶(p> 2)有限体积方法的网格的方法。我们通过假设基于局部重构的多项式误差度量来实现此目的。然后,我们使用傅立叶级数选择一个近似于我们的误差度量的度量函数。从理论上讲,该方法对于具有任意数量的变量和任意数量的尺寸的任何求解顺序都是有效的。我们同时使用二阶和三阶求解器,给出了围绕NACA-0012机翼的二维亚音速粘性和无粘性流的示例。这些测试案例表明,基于我们的度量标准的网格细化收敛到比统一细化要快得多的精确解决方案。对于亚音速粘性流,我们还表明各向异性细化比各向同性细化更有效。通过限制我们对跨音速无粘性流的误差测量的幅度,我们证明了即使在不连续的情况下,我们的度量也可以有效。我们还检查了使用二阶导数来估计三阶解的误差。尽管从理论上讲这不太合理,但我们发现最终的精度差异不大。

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