Features of the simulation of low velocity inviscid and viscous compressible gas flows are considered, and a finite volume discretization of gas dynamics equations at low Mach numbers on unstructured meshes is discussed. Preconditioning based on the use of physical variables is used to speed up the convergence of time marching to a steady state and to improve the accuracy of the steady state solution. The structure of the preconditioning matrix and the diagonalization of the Jacobian of the preconditioned system of equations are discussed. The capabilities of this approach are demonstrated using model gasdynamic simulations in a wide range of Mach numbers
AbstractThis paper presents a cell-centered high order finite volume scheme for the solution of the ...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
Preconditioning methods to accelerate convergence to a steady state for the incompressible fluid dyn...
Finite volume methods have been used to compute transonic flows by numerically solving the equations...
Finite volume methods have been used to compute transonic flows by numerically solving the equations...
The present report investigates the use of the unsteady compressible flow problems. For low speed f...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
The properties of a preconditioned, coupled, strongly implicit finite difference scheme for solving ...
A preconditioning scheme has been implemented into a three-dimensional viscous computational fluid d...
The present report investigates the use of the unsteady compressible flow equations in order to solv...
Local preconditioning for Eulerian-Eulerian gas-solid flow calculations with variable gas density is...
We consider the steady equations for a compressible fluid. For low speed flow the system is stiff s...
Acceleration methods are presented for solving the steady state incompressible equations. These syst...
The MSU TURBO code, distributed to U.S. engine companies by NASA Glenn, is a heavily used parallel c...
Approaching the incompressibility limit in CFD applications where compressible, density based soluti...
AbstractThis paper presents a cell-centered high order finite volume scheme for the solution of the ...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
Preconditioning methods to accelerate convergence to a steady state for the incompressible fluid dyn...
Finite volume methods have been used to compute transonic flows by numerically solving the equations...
Finite volume methods have been used to compute transonic flows by numerically solving the equations...
The present report investigates the use of the unsteady compressible flow problems. For low speed f...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
The properties of a preconditioned, coupled, strongly implicit finite difference scheme for solving ...
A preconditioning scheme has been implemented into a three-dimensional viscous computational fluid d...
The present report investigates the use of the unsteady compressible flow equations in order to solv...
Local preconditioning for Eulerian-Eulerian gas-solid flow calculations with variable gas density is...
We consider the steady equations for a compressible fluid. For low speed flow the system is stiff s...
Acceleration methods are presented for solving the steady state incompressible equations. These syst...
The MSU TURBO code, distributed to U.S. engine companies by NASA Glenn, is a heavily used parallel c...
Approaching the incompressibility limit in CFD applications where compressible, density based soluti...
AbstractThis paper presents a cell-centered high order finite volume scheme for the solution of the ...
We consider the steady-state equations for a compressible fluid. For low-speed flow, the system is s...
Preconditioning methods to accelerate convergence to a steady state for the incompressible fluid dyn...