Resolving chemically reacting flow using moving mesh method
We apply an adaptive mesh redistribution method to numerical simulation of chemically reacting ows. Our method consists of two independent parts: a ow solver and a mesh redistribution algorithm. We adopt a second-order upwind TVD and LU-SGS schemes for solving the Navier- Stokes equations with finite rate chemistry. The adaptive meshes are generated by solving elliptic equations, with the monitor function carefully designed to resolve the shock wave and the combustion front as well as the induction zone between them. Numerical simulations of supersonic ow past an axisymmetric projectile in premixed hydrogen/oxygen mixture are demonstrated. It is shown that the ow structures can be resolved satisfactorily on adaptive meshes.
adaptive mesh redistribution monitor function chemically reacting ow shock-induced combustion
Y.Li T.Fei W.Liu
Institute of Computational Mathematics and LSEC, Academy of Mathematics and Systems Science,Chinese Academy of Sciences, Beijing 100080, China
国际会议
The Fifth International Conference on Fluid Mechanics(第五届国际流体力学会议)
上海
英文
2007-08-15(万方平台首次上网日期,不代表论文的发表时间)