The oblique shock im**ing on the supersonic turbulent boundary layer leads to a mixing
layer and the emergence of large-scale coherent structures within the interaction zone which …

During the operation of hypersonic vehicles, a reciprocal coupling effect is manifested
between the inlet and the combustion chamber. This results in an unavoidable non …

Fluids at supercritical pressure (SCP) exhibit strong real-fluid effects near the pseudo-critical
point. These effects could modulate turbulence anisotropy and pose challenges to existing …