“…Downstream of the surface shock, the pressure is highest at the centre of the impingement zone as the axial flow velocity must decrease to zero. However, this stagnant, high pressure gas rapidly expands radially, diverting the flow into a wall jet [49,50]. Consequently, the shape of the surface shock is dictated by conservation of mass, energy, and momentum at the interface between the upstream supersonic expansion and the spatial profile of the downstream flow properties (direction, pressure, density, and temperature).…”