Численное исследование формирования псевдоскачка в канале

In this paper we present some results of pseudo-shock region formation in the channel of the ramjet air intake. Particularly, the influence of boundary layer thickness at inlet and back pressure in the outflow region (implemented via energy input) on the flow is studied. Simulation results show that these parameters can have crucial influence on the flow pattern and their correct accounting is of the great importance in validation with laboratory experiments.