Analytical study of the possibilities of controlling the parameters of shocks in supersonic flow around gas-permeable bodies

The possibility of controlling shock waves during high-speed flow around gas-permeable aerodynamic surfaces is studied. Numerical modeling of normal jet blowing from the body surface is carried out. The obtained results are compared with the results of the flow around a rigid (impenetrable) body in a plane setting. The change in gas-dynamic parameters and flow structure is determined when gas permeability occurs.