Implicit large-eddy simulation (ILES) of a shock wave/boundary-layer interaction (SBLI) was performed. Comparisons with experimental data showed a sensitivity of the current prediction to the modeling of the sidewalls. This was found to be common among various computational studies in the literature where periodic boundary conditions were used in the spanwise direction, as was the case in the present work. Thus, although the experiment was quasi-two-dimensional, the present simulation was determined to be two-dimensional. Quantities present in the exact equation of the Reynolds-stress transport, i.e., production, molecular diffusion, turbulent transport, pressure diffusion, pressure strain, dissipation, and turbulent mass flux were calculat...
A parametric study of Multiple Shock Wave Boundary Layer Interactions is presented in this paper. Al...
Reynolds Averaged Navier Stokes simulation (RANS) using the in-house CFD solver of Glasgow Universit...
The properties of 2-D shock wave/turbulent boundary layer interaction flows were calculated by using...
Implicit large-eddy simulation (ILES) of a shock wave/boundary-layer interaction (SBLI) was performe...
Large-eddy simulations are performed using wall-resolved mesh for a Mach 2.29 impinging shock wave/b...
AbstractIt is of great significance to improve the accuracy of turbulence models in shock-wave/bound...
Reynolds-averaged Navier-Stokes computations of a shock-wave/boundary-layer interaction (SWBLI) crea...
Shock wave boundary layer interactions (SBLIs) are physical phenomena which occur in many applicatio...
Shock wave boundary layer interactions occur in many aerospace applications, and of particular inter...
It is of great significance to improve the accuracy of turbulence models in shock-wave/boundary laye...
Shock boundary–layer interactions occur in many high-speed aerodynamic flows and they can have a not...
Shock wave turbulent boundary layer interactions (SWTBLI) commonly arise in turbomachinery and aeros...
Numerical solutions of the complete, time-averaged conservation equations using several eddy-viscosi...
This paper reports the wall-resolved large eddy simulations of shock-induced boundary layer separati...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
A parametric study of Multiple Shock Wave Boundary Layer Interactions is presented in this paper. Al...
Reynolds Averaged Navier Stokes simulation (RANS) using the in-house CFD solver of Glasgow Universit...
The properties of 2-D shock wave/turbulent boundary layer interaction flows were calculated by using...
Implicit large-eddy simulation (ILES) of a shock wave/boundary-layer interaction (SBLI) was performe...
Large-eddy simulations are performed using wall-resolved mesh for a Mach 2.29 impinging shock wave/b...
AbstractIt is of great significance to improve the accuracy of turbulence models in shock-wave/bound...
Reynolds-averaged Navier-Stokes computations of a shock-wave/boundary-layer interaction (SWBLI) crea...
Shock wave boundary layer interactions (SBLIs) are physical phenomena which occur in many applicatio...
Shock wave boundary layer interactions occur in many aerospace applications, and of particular inter...
It is of great significance to improve the accuracy of turbulence models in shock-wave/boundary laye...
Shock boundary–layer interactions occur in many high-speed aerodynamic flows and they can have a not...
Shock wave turbulent boundary layer interactions (SWTBLI) commonly arise in turbomachinery and aeros...
Numerical solutions of the complete, time-averaged conservation equations using several eddy-viscosi...
This paper reports the wall-resolved large eddy simulations of shock-induced boundary layer separati...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
A parametric study of Multiple Shock Wave Boundary Layer Interactions is presented in this paper. Al...
Reynolds Averaged Navier Stokes simulation (RANS) using the in-house CFD solver of Glasgow Universit...
The properties of 2-D shock wave/turbulent boundary layer interaction flows were calculated by using...