Abstract
A multigrid method for solving the compressible Navier Stokes equations is presented. The dimensionless conservation equations are discretized by a finite volume technique and time integration is performed by using a multistage explicit algorithm. Convergence to a steady state is enhanced by local time stepping, implicit smoothing of the residuals and the use of multiple grids. The method has been implemented in two different ways: firstly a cell centered and secondly a corner point formulation (i. e. the unknown variables are defined either at the center of a computational cell or at its vertices). Computed results are presented for laminar and turbulent two dimensional flows over airfoils.
| Original language | English (US) |
|---|---|
| Journal | AIAA Paper |
| State | Published - 1986 |
All Science Journal Classification (ASJC) codes
- General Engineering
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