宇航总体技术2024,Vol.8Issue(6) :33-41.DOI:10.20210/j.issn.2096-4080.2024.06.005

基于非结构网格的燃气流场算法程序实现及应用

Implementation and Application of Computing Program for Gas Flows

李航波 陈劲松 王帅
宇航总体技术2024,Vol.8Issue(6) :33-41.DOI:10.20210/j.issn.2096-4080.2024.06.005

基于非结构网格的燃气流场算法程序实现及应用

Implementation and Application of Computing Program for Gas Flows

李航波 1陈劲松 1王帅1
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作者信息

  • 1. 北京航天发射技术研究所,北京 100076
  • 折叠

摘要

利用有限体积法对非结构网格下的瞬态Euler方程进行离散,自主开发了基于密度基算法的流场计算程序,并在非结构网格下使用满足TVD(Total Variation Diminishing)性质的二阶格式得到界面上的变量值.采用 Roe-FDS 和 AUSM+(Advection Upstream Splitting Method+)迎风格式进行通量计算,并通过二维Sod管、前台阶激波反射算例验证了算法的可靠性.将算法推广至三维,并对冷态和热态空气自由喷流进行了计算,得到轴线马赫数分布曲线,对比得到不同格式的计算结果.结果表明,结合二阶格式的AUSM+算法在推广至三维非结构网格后耗散仍大于商业软件结果,但二阶Roe算法的结果耗散小于商业软件计算.

Abstract

The finite volume method is used to discretize the transient Euler equation on unstruc-tured grids.A flow field calculation program based on the density-based algorithm is developed,and the surface variables are obtained by using a second-order scheme satisfying the TVD property on unstructured grids.Roe-FDS and AUSM+upwind schemes are used to calculate the flux on the face,and the reliability of the algorithm is verified by classical examples.Then the program is extended to three-dimensional calculation.The flow of free jet is calculated,and the distribution of Mach number on the axis line is obtained.The calculation results of different algorithms are com-pleted.It shows that the dissipation of the AUSM+scheme combined with the second-order scheme is still greater than that of the calculation of Fluent,but the dissipation of the second-order Roe scheme is less than that of the calculation of Fluent.

关键词

燃气流场/TVD/AUSM+/Roe/非结构网格

Key words

Gas flow field/TVD/AUSM+/Roe/Unstructured grid

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出版年

2024
宇航总体技术

宇航总体技术

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