Mixing processes of supersonic flows in a model duct of a rocket scramjet engine

On the possible formation of a vortex flow in a supersonic inlet with three-dimensional compression

“…The available results of experimental and numerical studies show that the flow in the inlet and the channel is very complicated and exhibits numerous gasdynamic peculiarities [4][5][6][7][8]. Further experimental investigation of the parameters of 3D-compression air-intakes is topical for both a deeper understanding of the complicated gasdynamics of such devices and verification of the methods of numerical modeling of such flows.…”