Abstract:
A method of flow control in a two-dimensional hypersonic boundary layer under strong viscous-inviscid interaction is considered. The effect of blocking the process of transferring disturbances upstream due to a decrease in the propagation velocity of disturbances with a decrease in the temperature factor of the surface area is shown.
Keywords:asymptotic theory of viscous gas, controlling of flow, propagation of perturbations, viscous–inviscid interaction.