A new multigrid relaxation scheme, lower-upper symmetric successive overrelaxation (LU-SSOR) is developed for the steady-state solution of the Euler and Navier-Stokes equations. The scheme, which is based on central differences, does not require flux splitting for approximate Newton iteration. Application to transonic flow shows that the new method is efficient and robust. The vectorizable LU-SSOR scheme needs only scalar diagonal inversions
This paper describes a method for efficiently solving the steady-state Euler and Navier-Stokes equat...
Examined are some splitting techniques for low Mach number Euler flows. Shortcomings of some of the ...
The Navier-Stokes Computer is a multi-purpose parallel-processing supercomputer which is currently u...
Two methods are presented for inviscid transonic flows: unsteady Euler equations in a rotating frame...
A NEW multigrid relaxation scheme is developed for thesteady-state solution of the Euler and Navier-...
A consistent and efficient set of boundary conditions is developed for the multi-sweep space-marchin...
The cell-vertex schemes due to Ni and Jameson, et al. have been subjected to a theoretical analysis ...
A finite difference scheme for three-dimensional steady laminar incompressible flows is presented. T...
A multiple-grid algorithm for use in efficiently obtaining steady solutions to the Euler and Navier-...
The steady state Euler and Navier-Stokes equations are considered for both compressible and incompre...
The convergence characteristics of various approximate factorizations for the 3D Euler and Navier-St...
Future aircraft will eventually feature nonaxisymmetric or rectangular nozzles. Developing a three-d...
The 1980s may well be called the Euler era of applied aerodynamics. Computer codes based on discrete...
A multi-stage Runge-Kutta method is analyzed for solving the Euler equations exterior to an airfoil....
A coarse-grid correction algorithm has been implemented into an implicit upwind Euler solver and tes...
This paper describes a method for efficiently solving the steady-state Euler and Navier-Stokes equat...
Examined are some splitting techniques for low Mach number Euler flows. Shortcomings of some of the ...
The Navier-Stokes Computer is a multi-purpose parallel-processing supercomputer which is currently u...
Two methods are presented for inviscid transonic flows: unsteady Euler equations in a rotating frame...
A NEW multigrid relaxation scheme is developed for thesteady-state solution of the Euler and Navier-...
A consistent and efficient set of boundary conditions is developed for the multi-sweep space-marchin...
The cell-vertex schemes due to Ni and Jameson, et al. have been subjected to a theoretical analysis ...
A finite difference scheme for three-dimensional steady laminar incompressible flows is presented. T...
A multiple-grid algorithm for use in efficiently obtaining steady solutions to the Euler and Navier-...
The steady state Euler and Navier-Stokes equations are considered for both compressible and incompre...
The convergence characteristics of various approximate factorizations for the 3D Euler and Navier-St...
Future aircraft will eventually feature nonaxisymmetric or rectangular nozzles. Developing a three-d...
The 1980s may well be called the Euler era of applied aerodynamics. Computer codes based on discrete...
A multi-stage Runge-Kutta method is analyzed for solving the Euler equations exterior to an airfoil....
A coarse-grid correction algorithm has been implemented into an implicit upwind Euler solver and tes...
This paper describes a method for efficiently solving the steady-state Euler and Navier-Stokes equat...
Examined are some splitting techniques for low Mach number Euler flows. Shortcomings of some of the ...
The Navier-Stokes Computer is a multi-purpose parallel-processing supercomputer which is currently u...