A robust compact least-squares reconstruction method for compressible turbulent flow simulations of complex configurations

IF 5.3 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Jia YAN , Zhengyu NIU , Xiaoquan YANG , Jue DING , Xiaolong TANG , Peifeng WENG
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引用次数: 1

Abstract

For the second-order finite volume method, implicit schemes and reconstruction methods are two main algorithms which influence the robustness and efficiency of the numerical simulations of compressible turbulent flows. In this paper, a compact least-squares reconstruction method is proposed to calculate the gradients for the distribution of flow field variables approximation. The compactness of the new reconstruction method is reflected in the gradient calculation process. The geometries of the face-neighboring elements are no longer utilized, and the weighted average values at the centroid of the interfaces are used to calculate the gradients instead of the values at the centroid of the face-neighboring elements. Meanwhile, an exact Jacobian solving strategy is developed for implicit temporal discretization. The accurate processing of Jacobian matrix can extensively improve the invertibility of the Jacobian matrix and avoid introducing extra numerical errors. In addition, a modified Venkatakrishnan limiter is applied to deal with the shock which may appear in transonic flows and the applicability of the mentioned methods is enhanced further. The combination of the proposed methods makes the numerical simulations of turbulent flow converge rapidly and steadily with an adaptive increasing CFL number. The numerical results of several benchmarks indicate that the proposed methods perform well in terms of robustness, efficiency and accuracy, and have good application potential in turbulent flow simulations of complex configurations.

一种用于复杂结构可压缩湍流模拟的鲁棒紧致最小二乘重构方法
对于二阶有限体积法,隐式方案和重构方法是影响可压缩湍流数值模拟鲁棒性和效率的两种主要算法。本文提出了一种紧凑的最小二乘重构方法,用于计算流场变量分布近似的梯度。新重构方法的紧凑性体现在梯度计算过程中。在计算梯度时,不再使用相邻面元素的几何形状,而是使用界面中心点的加权平均值,而不是相邻面元素中心点的值。同时,为隐式时间离散化开发了精确的雅各布求解策略。对雅各布矩阵的精确处理可以大大提高雅各布矩阵的可逆性,避免引入额外的数值误差。此外,还采用了改进的 Venkatakrishnan 限幅器来处理跨音速流动中可能出现的冲击,从而进一步提高了上述方法的适用性。结合所提出的方法,湍流数值模拟可以随着 CFL 数的自适应增加而快速稳定地收敛。几个基准的数值结果表明,所提出的方法在鲁棒性、效率和精度方面表现良好,在复杂构型的湍流模拟中具有良好的应用潜力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics 工程技术-工程:宇航
CiteScore
10.00
自引率
17.50%
发文量
3080
审稿时长
55 days
期刊介绍: Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.
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