Euler方程的分裂型通量分裂双时间步隐式方法  

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

作　　者：董海涛[1] 陈喆[1] 刘福军[1] 

机构地区：[1]北京航空航天大学航空科学与工程学院,北京100191

出　　处：《北京航空航天大学学报》2015年第5期776-785,共10页Journal of Beijing University of Aeronautics and Astronautics

摘　　要：传统隐式方法有格式复杂、计算量大等缺点,在Euler方程的差分离散过程中,利用算子分裂思想,结合通量分裂法、双时间步法等隐式离散方法,构造了一种更简单的分裂型隐式计算方法.通过对典型空气动力学问题的计算,检验了该方法的有效性和可靠性,并对其性能做了具体讨论.该方法具有稳定性好、时间步长约束小等隐式格式的普遍优点,同时具有格式简单、程序易实现等优点;避免了传统隐式方法单步推进时的方程组常规求解及矩阵求逆过程,计算量小;比LU-SGS方法收敛速度快.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 equa- tions 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 dis- cussed 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.

关 键 词：EULER方程 算子分裂 通量分裂 双时间步 隐式方法 

分 类 号：O35[理学—流体力学]