Abstract:
The dynamics of two-dimensional flows of nonequilibrium gas is considered taking into account relaxation processes, viscosity and thermal conductivity. Based on the numerical gas-dynamic method MUSCL, a parallel computing algorithm is implemented, which allows studying nonlinear wave structures arising in a non-equilibrium medium due to the development of gas-dynamic instabilities with high spatial resolution. A significant increase (by 100–1000 times) in computing performance is shown when using parallel versions of the computing code for GPUs. Numerical modeling of shock-wave structures in a flat two-dimensional channel with injection of a supersonic jet of non-equilibrium gas is carried out.