Semi-implicit characteristic-based boundary treatment for acoustics in low Mach number flows

被引:3
作者
Moguen, Yann [1 ]
Bruel, Pascal [2 ,3 ]
Dick, Erik [1 ]
机构
[1] Univ Ghent, Dept Flow Heat & Combust Mech, B-9000 Ghent, Belgium
[2] Univ Pau & Pays Adour, CNRS, LMAP, UMR 5142, F-64013 Pau, France
[3] Inria CAGIRE Team, F-64013 Pau, France
关键词
Characteristic-based boundary conditions; Low Mach number flow; Semi implicit algorithm; Acoustics; DIRECT NUMERICAL-SIMULATION; DISSIPATION; SEQUEL; SCHEME; SPEEDS; AUSM;
D O I
10.1016/j.jcp.2013.08.019
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
For low Mach number flow calculation, when acoustic waves have to be captured, semi-implicit methods allow to avoid the time-step limitation that arises when explicit schemes are used. A method is suggested to solve the boundary equations so that the semi-implicitness of the algorithm is maintained, as well as its pressure-velocity coupling. This method is studied theoretically and numerically, in the low Mach number regime. Partially non-reflective characteristic-based boundary conditions, with the linear relaxation form suggested by Rudy and Strikwerda, [J. Comput. Phys. 36 (1980) 55-70], are considered. It is shown that their properties, well known in the framework of explicit schemes, are recovered with the proposed semi-implicit treatment and an acoustic CFL number significantly larger than unity. (c) 2013 Elsevier Inc. All rights reserved.
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页码:339 / 361
页数:23
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