This paper describes a method for efficiently solving the steady-state Euler and Navier-Stokes equations. Robustness is achieved through the use of an upwind TVD scheme for discretising the convective terms. The approximate solution is advanced in time implicitly and the linear system arising at each implicit step is solved using a Conjugate Gradient type method. The main emphasis of this paper is on the use of Jacobian matrices associated with a simpler spatial discretisation. This leads to better conditioned linear systems. The resulting method has lower memory and CPU-time requirements when compared with the one using exact Jacobians
A parallel Jacobian-free solver for supersonic flows on unstructured hybrid meshes is proposed. An e...
A coarse-grid correction algorithm has been implemented into an implicit upwind Euler solver and tes...
The 1980s may well be called the Euler era of applied aerodynamics. Computer codes based on discrete...
This paper describes a method for efficiently solving the steady-state Euler and Navier-Stokes equat...
Since residual vector in a control volume is the linear combination of inviscid and viscous flux vec...
Newton’s method for steady laminar flows over aerofoils is examined as a prelude to the study of mo...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...
Newton's method is developed for solving the 2-D Euler equations. The Euler equations are discretize...
An unfactored implicit time-marching method for the solution of the three dimensional Navier-Stokes...
In the present study, a scheme capable of solving very fast and robust complex nonlinear systems of ...
An efficient three-dimensionasl tructured solver for the Euler and Navier-Stokese quations is devel...
The objective of this study was to develop a high-resolution-explicit-multi-block numerical algorith...
An efficient implicit finite-difference algorithm for the gas dynamic equations utilizing matrix red...
Linearized alternating direction implicit (ADI) forms of a class of total variation diminishing (TVD...
A class of implicit upwind differencing methods for the compressible Navier-Stokes equations is desc...
A parallel Jacobian-free solver for supersonic flows on unstructured hybrid meshes is proposed. An e...
A coarse-grid correction algorithm has been implemented into an implicit upwind Euler solver and tes...
The 1980s may well be called the Euler era of applied aerodynamics. Computer codes based on discrete...
This paper describes a method for efficiently solving the steady-state Euler and Navier-Stokes equat...
Since residual vector in a control volume is the linear combination of inviscid and viscous flux vec...
Newton’s method for steady laminar flows over aerofoils is examined as a prelude to the study of mo...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...
Newton's method is developed for solving the 2-D Euler equations. The Euler equations are discretize...
An unfactored implicit time-marching method for the solution of the three dimensional Navier-Stokes...
In the present study, a scheme capable of solving very fast and robust complex nonlinear systems of ...
An efficient three-dimensionasl tructured solver for the Euler and Navier-Stokese quations is devel...
The objective of this study was to develop a high-resolution-explicit-multi-block numerical algorith...
An efficient implicit finite-difference algorithm for the gas dynamic equations utilizing matrix red...
Linearized alternating direction implicit (ADI) forms of a class of total variation diminishing (TVD...
A class of implicit upwind differencing methods for the compressible Navier-Stokes equations is desc...
A parallel Jacobian-free solver for supersonic flows on unstructured hybrid meshes is proposed. An e...
A coarse-grid correction algorithm has been implemented into an implicit upwind Euler solver and tes...
The 1980s may well be called the Euler era of applied aerodynamics. Computer codes based on discrete...