Well-resolved large-eddy simulations (LES) are performed in order to investigate flow phenomena
and turbulence structure of the boundary layer along a supersonic compression ramp. …

Large eddy simulations of shock wave/turbulent boundary layer interaction on a compression
ramp at the Mach number M a∞= 5 and Reynolds number R e∞= 14 000 are performed to …

… application in shock-induced separation control are studied using large-eddy simulation in
this paper. The base flow is the interaction of an oblique shock-wave generated by 8 wedge …

… We present wall-modelled large-eddy simulations (WLES) of oblique shock waves interacting
with the turbulent boundary layers (TBLs) (nominal δ99 = 5.4 mm and Reθ ≈ 1.4 × 104) …

… large eddy simulation was made of transonic flow over a two-dimensional bump where shock
wave turbulent boundary layer interaction … shock wave turbulent boundary layer interaction …

… shock wave–turbulent boundary-layer interaction. Results shown that these essentially 3-D
devices have a good control effect and lead to reduced stagnation pressure loss. Croker [10] …

… shock wave/turbulent boundary layer interaction have been published,6,7) but simulation
of the boundary layer transition induced by SWBLI is still a challenge for LES/DNS. Lawal and …

… Although basic understanding of flow physics of this interaction has been … shock-wave
turbulent boundary-layer interactions is still needed. In particular, if the structure of the interaction …

… flow properties, turbulence structure within the interaction region and unsteady shock dynamics
by analysing results from implicit large-eddy simulations. Details of the flow configuration …

… In this paper, the large eddy simulation is used to study the reflected shock/turbulent boundary
layer interaction with inlet Mach number Ma = 2.9 . The turbulent structure is analyzed and …