The use is considered of a multigrid method with central differencing to solve the Navier-Stokes equations for high speed flows. The time dependent form of the equations is integrated with a Runge-Kutta scheme accelerated by local time stepping and variable coefficient implicit residual smoothing. Of particular importance are the details of the numerical dissipation formulation, especially the switch between the second and fourth difference terms. Solutions are given for 2-D laminar flow over a circular cylinder and a 15 deg compression ramp
ia1 We consider the use of multigrid methods to solve the Euler equations for hypersonic flow. We co...
Summarization: The Navier-Stokes equations, that govern the motion of an incompressible or compressi...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...
The use of a multigrid method with central differencing to solve the Navier-Stokes equations for hyp...
A multigrid acceleration technique developed for solving 3-D Navier-Stokes equations for subsonic/tr...
The use of multigrid methods to solve the Euler equations for hypersonic flow is discussed. The stea...
Several multigrid schemes are considered for the numerical computation of viscous hypersonic flows. ...
Efficient acceleration techniques typical of explicit steady-state solvers are extended to time-accu...
Several multigrid schemes are considered for the numerical computation of viscous hypersonic flows. ...
A class of explicit multistage time-stepping schemes is used to construct an algorithm for solving t...
. The linearized Navier--Stokes equations are solved in 2D using a multigrid method where a semi-im...
l t Speolal Several multigrid schemes are considered for the numerical computation of viscous hypers...
The paper describes the results obtained from a multigrid accelerated Navier-Stokes solver. The meth...
A cell-vertex scheme for the Navier-Stokes equations, which is based on central difference approxima...
In steady hypersonic flow computations, Newton iteration as a local relaxation procedure and nonline...
ia1 We consider the use of multigrid methods to solve the Euler equations for hypersonic flow. We co...
Summarization: The Navier-Stokes equations, that govern the motion of an incompressible or compressi...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...
The use of a multigrid method with central differencing to solve the Navier-Stokes equations for hyp...
A multigrid acceleration technique developed for solving 3-D Navier-Stokes equations for subsonic/tr...
The use of multigrid methods to solve the Euler equations for hypersonic flow is discussed. The stea...
Several multigrid schemes are considered for the numerical computation of viscous hypersonic flows. ...
Efficient acceleration techniques typical of explicit steady-state solvers are extended to time-accu...
Several multigrid schemes are considered for the numerical computation of viscous hypersonic flows. ...
A class of explicit multistage time-stepping schemes is used to construct an algorithm for solving t...
. The linearized Navier--Stokes equations are solved in 2D using a multigrid method where a semi-im...
l t Speolal Several multigrid schemes are considered for the numerical computation of viscous hypers...
The paper describes the results obtained from a multigrid accelerated Navier-Stokes solver. The meth...
A cell-vertex scheme for the Navier-Stokes equations, which is based on central difference approxima...
In steady hypersonic flow computations, Newton iteration as a local relaxation procedure and nonline...
ia1 We consider the use of multigrid methods to solve the Euler equations for hypersonic flow. We co...
Summarization: The Navier-Stokes equations, that govern the motion of an incompressible or compressi...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...