机译:On the use of a two-layer model for large-eddy simulations of supersonic boundary layers with separation
Normandie Univ, CORIA UMR 6614, CNRS Univ, F-76000 Rouen, France;
Wall modeling; Supersonic Turbulent Boundary Layer (STBL); Large-Eddy Simulation (LES); Pressure gradient; Nozzle flow;