General difference approximations to the fluid dynamic equations require an artificial viscosity in order to converge to a steady state. This artificial viscosity serves two purposes. One is to suppress high frequency noise which is not damped by the central differences. The second purpose is to introduce an entropy-like condition so that shocks can be captured. These viscosities need a coefficient to measure the amount of viscosity to be added. In the standard scheme, a scalar coefficient is used based on the spectral radius of the Jacobian of the convective flux. However, this can add too much viscosity to the slower waves. Hence, it is suggested that a matrix viscosity be used. This gives an appropriate viscosity for each wave component....
A class of implicit upwind differencing methods for the compressible Navier-Stokes equations is desc...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
Wall functions, as used in the typical high Reynolds number k-epsilon turbulence model, can be imple...
Using a central difference scheme, it is necessary to add an artificial viscosity in order to reach ...
A class of numerical dissipation models for central-difference schemes constructed with second- and ...
We use central differences to solve the time dependent Euler equations. The schemes are all advanced...
Several algorithms for introducing artificial dissipation into a central difference approximation to...
The performance of different shock capturing viscosities has been examined using our general fluid m...
AbstractComparisons are made between various finite difference algorithms used for the numerical sol...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...
In this paper we consider high-order centered finite difference approximations of hyperbolic conserv...
The total variation diminishing (TVD) finite difference scheme can be interpreted as a Lax-Wendroff ...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
A fresh approach is taken to the embarrassingly difficult problem of adequately modeling simple pure...
An entropy correction method for the unsteady full potential equation is presented. The unsteady pot...
A class of implicit upwind differencing methods for the compressible Navier-Stokes equations is desc...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
Wall functions, as used in the typical high Reynolds number k-epsilon turbulence model, can be imple...
Using a central difference scheme, it is necessary to add an artificial viscosity in order to reach ...
A class of numerical dissipation models for central-difference schemes constructed with second- and ...
We use central differences to solve the time dependent Euler equations. The schemes are all advanced...
Several algorithms for introducing artificial dissipation into a central difference approximation to...
The performance of different shock capturing viscosities has been examined using our general fluid m...
AbstractComparisons are made between various finite difference algorithms used for the numerical sol...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...
In this paper we consider high-order centered finite difference approximations of hyperbolic conserv...
The total variation diminishing (TVD) finite difference scheme can be interpreted as a Lax-Wendroff ...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
A fresh approach is taken to the embarrassingly difficult problem of adequately modeling simple pure...
An entropy correction method for the unsteady full potential equation is presented. The unsteady pot...
A class of implicit upwind differencing methods for the compressible Navier-Stokes equations is desc...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
Wall functions, as used in the typical high Reynolds number k-epsilon turbulence model, can be imple...