turning angles for individual facets of 22.5° and 30° has been conducted at an incident
shock Mach number of 1.5. The features of the near wall flow have been identified and the
early development of the flow around the wall was considered. For the Mach 1.5 case, the
expansion generated at each corner was shown to have a marked effect on the separation
shear layers formed after each corner. More work needs to be done using a less …