Stable Runge-Kutta discontinuous Galerkin solver for hypersonic rarefied gaseous flow based on 2D Boltzmann kinetic model equations
distribution functions、kinetic equation、relaxation term、hypersonic flow、current limiter、Mach number、shock wave、shock tube
38
O241.82;O356;O552.3(计算数学)
the National Natural Science Foundation of China 11302017
2017-05-03(万方平台首次上网日期,不代表论文的发表时间)
共20页
343-362