Implicit methods were developed and tested for unstructured mesh computations. The approximate system which arises from the Newton linearization of the nonlinear evolution operator is solved by using the preconditioned GMRES (Generalized Minimum Residual) technique. Three different preconditioners were studied, namely, the incomplete LU factorization (ILU), block diagonal factorization, and the symmetric successive over relaxation (SSOR). The preconditioners were optimized to have good vectorization properties. SSOR and ILU were also studied as iterative schemes. The various methods are compared over a wide range of problems. Ordering of the unknowns, which affects the convergence of these sparse matrix iterative methods, is also studied. R...
Efficient iterative solution methods are being developed for the numerical solution of two- and thre...
This study presents a time-marching, density-based flow solution method at all speeds for Euler and ...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...
An implicit code for computing inviscid and viscous incompressible flows on unstructured grids is de...
An implicit code for computing inviscid and viscous incompressible flows on unstructured grids is de...
An implicit method for the computation of unsteady flows on unstructured grids is presented. Followi...
For a computational flow simulation tool to be useful in a design environment, it must be very robus...
A mesh-vertex finite volume scheme for solving the Euler equations on triangular unstructured meshes...
Implicit methods based on the Newton’s rootfinding algorithm are receiving an increasing attention f...
Implicit methods based on the Newton’s rootfinding algorithm are receiving an increasing attention f...
Implicit methods based on the Newton’s rootfinding algorithm are receiving an increasing attention f...
Linearization of the non-linear systems arising from fully implicit schemes in computational fluid...
The development of implicit schemes for obtaining steady state solutions to the Euler and Navier-Sto...
The emphasis of this thesis is to improve the efficiency of unsteady computation of high Reynolds nu...
The development of efficient iterative solution methods for the numerical solution of two- and three...
Efficient iterative solution methods are being developed for the numerical solution of two- and thre...
This study presents a time-marching, density-based flow solution method at all speeds for Euler and ...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...
An implicit code for computing inviscid and viscous incompressible flows on unstructured grids is de...
An implicit code for computing inviscid and viscous incompressible flows on unstructured grids is de...
An implicit method for the computation of unsteady flows on unstructured grids is presented. Followi...
For a computational flow simulation tool to be useful in a design environment, it must be very robus...
A mesh-vertex finite volume scheme for solving the Euler equations on triangular unstructured meshes...
Implicit methods based on the Newton’s rootfinding algorithm are receiving an increasing attention f...
Implicit methods based on the Newton’s rootfinding algorithm are receiving an increasing attention f...
Implicit methods based on the Newton’s rootfinding algorithm are receiving an increasing attention f...
Linearization of the non-linear systems arising from fully implicit schemes in computational fluid...
The development of implicit schemes for obtaining steady state solutions to the Euler and Navier-Sto...
The emphasis of this thesis is to improve the efficiency of unsteady computation of high Reynolds nu...
The development of efficient iterative solution methods for the numerical solution of two- and three...
Efficient iterative solution methods are being developed for the numerical solution of two- and thre...
This study presents a time-marching, density-based flow solution method at all speeds for Euler and ...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...