Abstract:
We propose a physical and mathematical model of turbulent combustion subsonic gas jet of fuel
flowing into a space with air. Processes are described by the averaged equations of the boundary
layer model of turbulent viscosity and diffusion model of combustion. As models of turbulent
viscosity two-parameter model are made famous $k$-$\varepsilon$ and $k$-$\omega$. The comparison of numerical results with experimental data on the averaged and pulsating flow characteristics is presented.