Monotone integrated large eddy simulations for supersonic boundary layer flows

Monotone integrated large eddy simulation (MILES) has been carried out to simulate supersonic turbulent boundary layer flows for relatively high Reynolds numbers. Two Riemann solver based methods, Osher’s and Roe’s schemes, were tested along with a MUSCL scheme to investigate their suitability for MILES simulation. The effects of different limiters used in the MUSCL scheme were also tested regarding the MILES simulations.