Physical properties of the flow in the separation region for three-dimensional interaction of a boundary layer with a shock wave

Interaction between an Inclined Shock and Boundary and High-Entropy Layers on a Flat Plate

“…Finally, at the end of the sixties essentially three-dimensional interference flows, for example, on a plate ahead of a cylindrical obstacle, were investigated [17][18][19][20]. These investigations showed that a supersonic flow closed by a shock can develop inside the three-dimensional separation zone.…”

Calculation of the Flow Pattern and the Heat Fluxes in the Interaction of a Shock Wave with a Cylinder in a Supersonic Flow

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The problem of determining the mechanical and thermal action on a cylinder in a supersonic flow with account for the interference between an incident shock and the detached bow shock has been studied extensively, both experimentally and theoretically, in the last few decades [1][2][3][4][5][6][7][8][9][10][11][12]. A fairly complete survey can be found in monograph [12].

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“…Such flows were studied in detail in experiments [3][4][5][6]. The technique for calculating the peak pressure and heat transfer levels proposed above is extended to this case below.…”