Direct numerical simulations have been conducted to study the passage of a turbulent spot through a shock-induced separation bubble. Localized blowing is used to trip the boundary layer well upstream of the shock impingement, leading to mature turbulent spots at impingement, with a length comparable to the length of the separation zone. Interactions are simulated at free stream Mach numbers of two and four, for isothermal (hot) wall boundary conditions. The core of the spot is seen to tunnel through the separation bubble, leading to a transient reattachment of the flow. Recovery times are long due to the influence of the calmed region behind the spot. The propagation speed of the trailing interface of the spot decreases during the interacti...
Direct simulation of an isolated turbulent spot in a compressible isothermal wall boundary-layer flo...
The interaction of a shock wave and boundary layer often occurs in high speed flows. For sufficientl...
Transonic shock wave/boundary layer interaction over a wall-mounted bump was investigated with speci...
Direct numerical simulations have been performed to study the dynamics of isolated turbulent spots i...
The growth and breakdown of localised disturbances into a turbulent spot in a Mach 2 boundary-layer ...
The complex transition flow physics associated with the merging of turbulent spots in a Mach 2 bound...
The growth and breakdown of localised disturbances into a turbulent spot in a Mach 2 boundary-layer ...
Shock waves generated at different parts of vehicle interact with the boundary layer over the surfac...
This thesis presents a joint experimental/CFD investigation of shock-induced boundary layer separati...
Numerical simulations of an oblique shock interacting with a compressible laminar boundary layer are...
The compressible Navier–Stokes equations are solved for turbulentspots in otherwise laminar boundary...
AbstractThe compressible Navier–Stokes equations are solved for turbulent spots in otherwise laminar...
This study conducted a direct numerical simulation of an incident shock wave impinging at an angle o...
Direct numerical simulations of incident shock wave and supersonic turbulent boundary layer interact...
Shock-Boundary Layer Interaction (SBLI) often occurs in supersonic/hypersonic flow fields. Especiall...
Direct simulation of an isolated turbulent spot in a compressible isothermal wall boundary-layer flo...
The interaction of a shock wave and boundary layer often occurs in high speed flows. For sufficientl...
Transonic shock wave/boundary layer interaction over a wall-mounted bump was investigated with speci...
Direct numerical simulations have been performed to study the dynamics of isolated turbulent spots i...
The growth and breakdown of localised disturbances into a turbulent spot in a Mach 2 boundary-layer ...
The complex transition flow physics associated with the merging of turbulent spots in a Mach 2 bound...
The growth and breakdown of localised disturbances into a turbulent spot in a Mach 2 boundary-layer ...
Shock waves generated at different parts of vehicle interact with the boundary layer over the surfac...
This thesis presents a joint experimental/CFD investigation of shock-induced boundary layer separati...
Numerical simulations of an oblique shock interacting with a compressible laminar boundary layer are...
The compressible Navier–Stokes equations are solved for turbulentspots in otherwise laminar boundary...
AbstractThe compressible Navier–Stokes equations are solved for turbulent spots in otherwise laminar...
This study conducted a direct numerical simulation of an incident shock wave impinging at an angle o...
Direct numerical simulations of incident shock wave and supersonic turbulent boundary layer interact...
Shock-Boundary Layer Interaction (SBLI) often occurs in supersonic/hypersonic flow fields. Especiall...
Direct simulation of an isolated turbulent spot in a compressible isothermal wall boundary-layer flo...
The interaction of a shock wave and boundary layer often occurs in high speed flows. For sufficientl...
Transonic shock wave/boundary layer interaction over a wall-mounted bump was investigated with speci...