An efficient algorithm is presented for the solution of the steady Euler equations of gas dynamics. The scheme is based on solving linearised Riemann problems approximately and in more than one dimension incorporates operator splitting. The scheme is applied to a standard test problem of flow down a channel containing a circular arc bump for three different mesh sizes
This paper considers the streamline-upwind Petrov/Galerkin (SUPG) method applied to the compressible...
An unstructured, shock-fitting algorithm, originally developed to simulate steady flows, has being f...
An unstructured, shock-fitting algorithm, originally developed to simulate steady flows, has being f...
AbstractAn efficient algorithm is presented for the solution of the steady Euler equations of gas dy...
AbstractAn efficient algorithm is presented for the solution of the steady Euler equations of gas dy...
A finite difference scheme based on flux difference splitting is presented for the solution of the E...
AbstractA finite difference scheme based on flux difference splitting is presented for the solution ...
A numerical scheme is presented for the solution of the Euler equations of compressible flow of a ga...
AbstractA finite difference scheme based on flux difference splitting is presented for the solution ...
This report treats the development of a shock tube solver for the simulation of flows described by ...
Three topics on modern shock capturing methods for the time-dependent Euler equations of Gas Dynamic...
The solution of the compressible Euler equations involves, in some problems, development of disconti...
The development of shock-capturing finite difference methods for hyperbolic conservation laws has be...
A non-uniform mesh scheme is presented for the computation of compressible flows governed by the Eul...
In many technical applications it is necessary to compute a numerical solution of complex flow probl...
This paper considers the streamline-upwind Petrov/Galerkin (SUPG) method applied to the compressible...
An unstructured, shock-fitting algorithm, originally developed to simulate steady flows, has being f...
An unstructured, shock-fitting algorithm, originally developed to simulate steady flows, has being f...
AbstractAn efficient algorithm is presented for the solution of the steady Euler equations of gas dy...
AbstractAn efficient algorithm is presented for the solution of the steady Euler equations of gas dy...
A finite difference scheme based on flux difference splitting is presented for the solution of the E...
AbstractA finite difference scheme based on flux difference splitting is presented for the solution ...
A numerical scheme is presented for the solution of the Euler equations of compressible flow of a ga...
AbstractA finite difference scheme based on flux difference splitting is presented for the solution ...
This report treats the development of a shock tube solver for the simulation of flows described by ...
Three topics on modern shock capturing methods for the time-dependent Euler equations of Gas Dynamic...
The solution of the compressible Euler equations involves, in some problems, development of disconti...
The development of shock-capturing finite difference methods for hyperbolic conservation laws has be...
A non-uniform mesh scheme is presented for the computation of compressible flows governed by the Eul...
In many technical applications it is necessary to compute a numerical solution of complex flow probl...
This paper considers the streamline-upwind Petrov/Galerkin (SUPG) method applied to the compressible...
An unstructured, shock-fitting algorithm, originally developed to simulate steady flows, has being f...
An unstructured, shock-fitting algorithm, originally developed to simulate steady flows, has being f...