吉林大学学报(理学版) ›› 2020, Vol. 58 ›› Issue (6): 1371-1377.

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一种求解Euler方程的高阶格式

任琴琴1, 郑秋亚1, 梁益华2   

  1. 1. 长安大学 理学院, 西安 710064; 2. 中国航空计算技术研究所 航空气动力数值模拟重点实验室, 西安 710068
  • 出版日期:2020-11-18 发布日期:2020-11-26
  • 通讯作者: 郑秋亚muzizh_2006@126.com

A Higher Order Scheme for Solving Euler Equations

REN Qinqin1, ZHENG Qiuya1, LIANG Yihua2   

  1. 1. School of Science, Chang’an University, Xi’an 710064, China;
    2. Aeronautical Laboratory of Computational Fluid Dynamics, Aeronautics Computing Technique Research Institute, Xi’an 710068, China
  • Online:2020-11-18 Published:2020-11-26

摘要: 将总能对流迎风和分压(E-CUSP)格式与WENO-η-格式耦合给出一种新格式(记为E-CUSP-WENO-η), 解决了一维激波管问题. 数值模拟结果表明: 新格式对接触间断和激波的捕捉更精确, 其中带有高阶最优全局光滑因子的新格式(E-CUSP-WENO-η(τopt7))数值耗散最小; 耦合的新格式可以更陡峭地捕捉到激波, 且计算结果精度高, 稳定性好.

关键词: Euler方程, 计算流体力学, 总能对流迎风和分压格式, 加权本质无振荡格式, 光滑因子

Abstract: By coupling the total energy convective upwind and split pressure (E-CUSP) scheme with the WENO-η scheme, we gave a new scheme (E-CUSP-WENO-η) to solve the one-dimensional shock tube problem. The numerical simulation results show that the new scheme is more accurate in capturing contact discontinuities and shock waves, among which the new scheme (E-CUSP-WENO-η(τopt7)) with higher order optimal global smoothness factor has the least numerical dissipation. The coupled new scheme can capture shock wave more steeply, and the calculation results are accurate and stable.

Key words: Euler equation, computational fluid dynamics, total energy convective upwind and split pressure schemes, weighted essentially non-oscillatory schemes, smoothness factor

中图分类号: 

  • O242