气体动理学统一算法的隐式方法研究

毛枚良; 江定武; 李锦; 邓小刚

doi:10.6052/0459-1879-14-408

气体动理学统一算法的隐式方法研究

doi: 10.6052/0459-1879-14-408

毛枚良^1,2, ,,
江定武²,
李锦²,
邓小刚³

1.
中国空气动力研究与发展中心空气动力学国家重点实验室, 绵阳621000
2. 中国空气动力研究与发展中心计算空气动力研究所, 绵阳621000
3. 国防科学技术大学, 长沙410073

基金项目: 国家自然科学基金(11402287)、空气动力学国家重点实验室研究基金(SKLA2015-1-2)资助项目.

详细信息

通讯作者:
毛枚良,研究员,主要研究方向:复杂流动数值模拟方法及应用.E-mail:l219@163.com

中图分类号: V211.3
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出版历程
- 收稿日期: 2014-12-19
- 修回日期: 2015-06-06
- 刊出日期: 2015-09-18

STUDY ON IMPLICIT IMPLEMENTATION OF THE UNIFIED GAS KINETIC SCHEME

1.
State Key Laboratory of Aerodynamics , China Aerodynamics Research and Development Center, Mianyang 621000, China
2. Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
3. National University of Defense Technology, Changsha 410073, China

Funds: The project was supported by the National Natural Science Fundation of China(11402287) and Study Fund of State Key Laboratory of Aerodynamics (SKLA2015-1-2).

摘要

摘要: 目前的气体动理学统一算法(unified gas kinetic scheme, 简称UGKS) 在求解高速流动问题时的计算效率,难以满足求解复杂工程问题的需求. 为了提高该算法的计算效率, 本文对模型方程的对流项和碰撞项进行了隐式处理, 并针对UGKS 界面通量与演化时间相关的特点, 引入了演化时间平均界面通量, 通过对控制方程矩阵进行近似LU 分解(lower-upper decomposition), 实现了隐式UGKS. 不同来流马赫数的圆柱绕流算例测试表明, 只要演化时间选取得当, 隐式方法可以得到与显式方法完全相同的结果, 且计算效率可以提高1~2 个量级.
- 气体动理学统一算法 /
- 隐式方法 /
- 加速收敛
Abstract: The current explicit unified gas kinetic scheme (UGKS) is very time-consuming for high speed flows due to the massive phase space mesh demand, which is a bottleneck for complex engineering problems. In order to improve the efficiency, the motion and collision term in the model equation is implicitly treated and the evolving time averaged flux across the cell interface is introduced, then the implicit UGKS can be obtained applying the approximate LU decomposition on the matrix of the governing equations. The tests on the flows over a cylinder with different freestream Mach numbers show that the implicit method can give the same result as the original explicit method with a properly chosen evolving time step. Meanwhile, the computational efficiency can be improved by 1-2 orders.
- unified gas kinetic scheme /
- implicit method /
- convergence acceleration

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参考文献(25)

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