Split-type implicit scheme using flux splitting and dual-time step for euler equations

被引:0
作者
Dong, Haitao [1 ]
Chen, Zhe [1 ]
Liu, Fujun [1 ]
机构
[1] School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing
来源
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2015年 / 41卷 / 05期
关键词
Dual-time step; Euler equations; Flux vector splitting; Implicit scheme; Operator splitting;
D O I
10.13700/j.bh.1001-5965.2014.0326
中图分类号
学科分类号
摘要
There are some shortcomings of the traditional implicit schemes such as complex forms and large amount of computations. Using the idea of operator splitting combining with implicit discrete schemes-flux vector splitting and dual-time step scheme-a simpler split-type implicit difference scheme for Euler equations was developed. The validity and reliability of the new implicit scheme were verified by performing numerical experiments on some typical problems in aerodynamics, and the properties of the new scheme were discussed in detail at the same time. The new scheme has common advantages of good stability and few constraints on time step just like other implicit schemes. In addition, the new scheme has the following advantages: it has simple formulas; it is easy for programming; it needs smaller amount of computations by avoiding solving systems of equations and doing inverse matrix operation compared with conventional implicit schemes in single time step; it has faster convergence rate compared with LU-SGS scheme. ©, 2015, Beijing University of Aeronautics and Astronautics (BUAA). All right reserved.
引用
收藏
页码:776 / 785
页数:9
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