Abstract
For subsonic flows and upwind-discretized, linearized 1-D Euler equations, the smoothing behavior of multigrid-accelerated point Gauss-Seidel relaxation is analyzed. Error decay by convection across domain boundaries is also discussed. A fix to poor convergence rates at low Mach numbers is sought in replacing the point relaxation applied to unconditioned Euler equations, by locally implicit "time"-stepping applied to preconditioned Euler equations. The locally implicit iteration step is optimized for good damping of high-frequency errors. Numerical inaccuracy at low Mach numbers is also addressed.
| Original language | English |
|---|---|
| Pages (from-to) | 127-144 |
| Journal | Advances in Computational Mathematics |
| Volume | 4 |
| Issue number | 1 |
| DOIs | |
| Publication status | Published - 1995 |
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