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...
A numerical method for two-dimensional incompressible viscous fluid flows is tested on the diffusion...
March 1989Originally issued as: Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aer...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
Many Navier-Stokes codes require that the governing equations be written in conservation form with a...
A spatially developing supersonic adiabatic flat plate boundary layer flow (at M-infinity=2.25 and R...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
UnrestrictedIn the first part of this report, the effects of numerical dissipation presented in a tu...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
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 major problem in modeling of turbulent supersonic flows is the correct assessment of viscous-invis...
The accuracy of numerical solutions for the incompressible turbulent boundary layer past a flat plat...
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/...
One of the key factors in simulating realistic wall-bounded flows at high Reynolds numbers is the se...
A numerical method for two-dimensional incompressible viscous fluid flows is tested on the diffusion...
March 1989Originally issued as: Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aer...
ABSTRACT: The present work is primarily concerned with studying the effects of artificial dissipatio...
Many Navier-Stokes codes require that the governing equations be written in conservation form with a...
A spatially developing supersonic adiabatic flat plate boundary layer flow (at M-infinity=2.25 and R...
In this paper the artificial compressibility flux Discontinuous Galerkin (DG) method for the solutio...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
UnrestrictedIn the first part of this report, the effects of numerical dissipation presented in a tu...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
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 major problem in modeling of turbulent supersonic flows is the correct assessment of viscous-invis...
The accuracy of numerical solutions for the incompressible turbulent boundary layer past a flat plat...
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/...
One of the key factors in simulating realistic wall-bounded flows at high Reynolds numbers is the se...
A numerical method for two-dimensional incompressible viscous fluid flows is tested on the diffusion...
March 1989Originally issued as: Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aer...