ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipation and of certain diffusive terms in the turbulence model formulation on the capability of representing turbulent boundary layer flows. The flows of interest in the present case are assumed to be adequately represented by the compressible Reynolds-averaged Navier-Stokes equations, and the Spalart-Allmaras eddy viscosity model is used for turbulence closure. The equations are discretized in the context of a general purpose, density-based, unstructured grid finite volume method. Spatial discretization is based on the Steger-Warming flux vector splitting scheme and temporal discretization uses a backward Euler point-implicit integration. The work...
One of the key factors in simulating realistic wall-bounded flows at high Reynolds numbers is the se...
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/...
A major problem in modeling of turbulent supersonic flows is the correct assessment of viscous-invis...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
UnrestrictedIn the first part of this report, the effects of numerical dissipation presented in a tu...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
Many Navier-Stokes codes require that the governing equations be written in conservation form with a...
The quantitative measure of dissipative properties of different numerical schemes is crucial to comp...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
University of Minnesota Ph.D. dissertation. February 2012. Major: Aerospace Engineering and Mechanic...
International audienceWhen high Reynolds turbulent flows are combined with complex and large size ge...
A spatially developing supersonic adiabatic flat plate boundary layer flow (at M-infinity=2.25 and R...
A numerical method for two-dimensional incompressible viscous fluid flows is tested on the diffusion...
The simulation of turbulent flows by means of computational fluid dynamics is highly challenging. Th...
Physical discontinuities, such as shocks and interfaces occur commonly in fluid mechanics. The empha...
One of the key factors in simulating realistic wall-bounded flows at high Reynolds numbers is the se...
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/...
A major problem in modeling of turbulent supersonic flows is the correct assessment of viscous-invis...
AbstrAct: The present work is primarily concerned with studying the effects of artificial dissipatio...
UnrestrictedIn the first part of this report, the effects of numerical dissipation presented in a tu...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
Many Navier-Stokes codes require that the governing equations be written in conservation form with a...
The quantitative measure of dissipative properties of different numerical schemes is crucial to comp...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
University of Minnesota Ph.D. dissertation. February 2012. Major: Aerospace Engineering and Mechanic...
International audienceWhen high Reynolds turbulent flows are combined with complex and large size ge...
A spatially developing supersonic adiabatic flat plate boundary layer flow (at M-infinity=2.25 and R...
A numerical method for two-dimensional incompressible viscous fluid flows is tested on the diffusion...
The simulation of turbulent flows by means of computational fluid dynamics is highly challenging. Th...
Physical discontinuities, such as shocks and interfaces occur commonly in fluid mechanics. The empha...
One of the key factors in simulating realistic wall-bounded flows at high Reynolds numbers is the se...
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/...
A major problem in modeling of turbulent supersonic flows is the correct assessment of viscous-invis...