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A General Approach to Vorticity Confinement Development for High-Order Flow Solvers

机译:高阶流求解器涡度约束发展的一般方法

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The vortieity confinement technique is analyzed for a family of flow solvers based on upwind-biased differentiation schemes. Treating the necessary confinement level as a numerical error leads to a new technique for developing advanced confinement terms when the basic formulation is unable to preserve the vortex properties. It is show that for third- and fifth-order upwind-biased solvers, the error in vortex convection is substantially different than what is seen in a simple first-order scheme, explaining the original difficulty in developing a confinement term that is independent of grid density, vortex strength, and convection Mach number for these schemes. A functional confinement term is shown for the first-order scheme, and the difficulties in developing high-quality parameters for the higher-order schemes are discussed.
机译:基于迎风偏微分法,分析了一系列流动求解器的涡度限制技术。当基本公式无法保留涡旋特性时,将必要的约束水平视为数值误差会导致开发新的高级约束项的新技术。结果表明,对于三阶和五阶迎风偏向求解器,涡流对流的误差与简单的一阶方案中所观察到的有很大不同,这说明了开发独立于网格的约束项的原始困难这些方案的密度,涡旋强度和对流马赫数。给出了一阶方案的功能限制项,并讨论了为高阶方案开发高质量参数的困难。

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