Abstract
Third-order and fifth-order upwind compact finite difference schemes based on flux-difference splitting are proposed for solving the incompressible Navier-Stokes equations in conjunction with the artificial compressibility (AC) method. Since the governing equations in the AC method are hyperbolic, fluxdifference splitting (FDS) originally developed for the compressible Euler equations can be used. In the present upwind compact schemes, the split derivatives for the convective terms at grid points are linked to the differences of split fluxes between neighboring grid points, and these differences are computed by using FDS. The viscous terms are approximated with a sixth-order central compact scheme. Comparisons with 2D benchmark solutions demonstrate that the present compact schemes are simple, efficient, and high-order accurate.
| Original language | English |
|---|---|
| Pages (from-to) | 552-568 |
| Number of pages | 17 |
| Journal | International Journal for Numerical Methods in Fluids |
| Volume | 61 |
| Issue number | 5 |
| DOIs | |
| State | Published - Oct 2009 |
| Externally published | Yes |
Keywords
- Artificial compressibility
- Backward facing step
- Flux-difference splitting
- Incompressible Navier-Stokes equation
- Lid-driven cavity flow
- Upwind compact difference
ASJC Scopus subject areas
- Computational Mechanics
- Mechanics of Materials
- Mechanical Engineering
- Computer Science Applications
- Applied Mathematics