Turbulence statistics in a highly supersonic boundary layer downstream of an incident shock wave

In this work, the turbulence statistics in highly supersonic boundary layers downstream of an incident shock wave are investigated by DNS. The objective is to examine the transformations and scaling laws of spatially evolving highly supersonic boundary layers with a canonical setup. This can allow for the development of efficient reduced-order models for turbulent boundary layers, such as wall-modeled large-eddy simulations (WMLES).