Direct numerical simulation (DNS) and inviscid linear analysis (LIA) are used to study the interaction of a normal Mach 1.5 shock wave and isotropic turbulence. The influence of the nature of the incoming turbulence on the interaction is emphasized. The presence of upstream entropy fluctuations enhance the amplification of the turbulent kinetic energy and transverse vorticity variance across the shock compared to the solenoidal (pure vorticity) case. More reduction of the transverse Taylor microscale is also observed in the vorticity-entropy case while no influence can be seen on the longitudinal microscale. When acoustic and vortical fluctuations are associated upstream, less amplification of the turbulent kinetic energy, less reduction of...
Development of improved turbulence closure models for compressible fluid flow simulations requires b...
The focus of this presentation is upon results from direct numerical simulations (DNS) of a range of...
Direct numerical simulation is used to study the in-teraction of a Mach 1.5 shock wave and various t...
Direct numerical simulation is used to study the interaction of a Mach 1.5 shock wave and various ty...
Direct numerical simulation is used to study the interaction of a Mach 1.5 shock wave and various ty...
Direct numerical simulation (DNS) and linear analysis (LIA) of isotropic turbulence interacting with...
The interaction of turbulence with shock waves, while very common in nature and engineered systems, ...
Turbulent velocity and thermal correlations from direct numerical simulation data of a ...
Several direct simulations of 3-D homogeneous, compressible turbulence are presented with emphasis o...
The interaction of turbulence with a shock wave is a fundamental prob-lem in fluid mechanics relevan...
This work is a small extension of NACA studies of the early fifties that predicted amplification of ...
A Chebyshev-Fourier discretization with shock fitting is used to solve the unsteady Euler equations....
A nearly homogeneous nearly isotropic compressible turbulent flow interacting with a normal shock wa...
The canonical problem of a nearly stationary, nearly planar shockwave passing through isotropic turb...
The streamwise back and forth movement of the separation bubble, triggered by the shock wave/boundar...
Development of improved turbulence closure models for compressible fluid flow simulations requires b...
The focus of this presentation is upon results from direct numerical simulations (DNS) of a range of...
Direct numerical simulation is used to study the in-teraction of a Mach 1.5 shock wave and various t...
Direct numerical simulation is used to study the interaction of a Mach 1.5 shock wave and various ty...
Direct numerical simulation is used to study the interaction of a Mach 1.5 shock wave and various ty...
Direct numerical simulation (DNS) and linear analysis (LIA) of isotropic turbulence interacting with...
The interaction of turbulence with shock waves, while very common in nature and engineered systems, ...
Turbulent velocity and thermal correlations from direct numerical simulation data of a ...
Several direct simulations of 3-D homogeneous, compressible turbulence are presented with emphasis o...
The interaction of turbulence with a shock wave is a fundamental prob-lem in fluid mechanics relevan...
This work is a small extension of NACA studies of the early fifties that predicted amplification of ...
A Chebyshev-Fourier discretization with shock fitting is used to solve the unsteady Euler equations....
A nearly homogeneous nearly isotropic compressible turbulent flow interacting with a normal shock wa...
The canonical problem of a nearly stationary, nearly planar shockwave passing through isotropic turb...
The streamwise back and forth movement of the separation bubble, triggered by the shock wave/boundar...
Development of improved turbulence closure models for compressible fluid flow simulations requires b...
The focus of this presentation is upon results from direct numerical simulations (DNS) of a range of...
Direct numerical simulation is used to study the in-teraction of a Mach 1.5 shock wave and various t...