Abstract
This paper presents a new version of the upwind compact finite difference scheme for solving the incompressible Navier-Stokes equations in generalized curvilinear coordinates. The artificial compressibility approach is used, which transforms the elliptic-parabolic equations into the hyperbolic-parabolic ones so that flux difference splitting can be applied. The convective terms are approximated by a third-order upwind compact scheme implemented with flux difference splitting, and the viscous terms are approximated by a fourth-order central compact scheme. The solution algorithm used is the Beam-Warming approximate factorization scheme. Numerical solutions to benchmark problems of the steady plane Couette-Poiseuille flow, the lid-driven cavity flow, and the constricting channel flow with varying geometry are presented. The computed results are found in good agreement with established analytical and numerical results. The third-order accuracy of the scheme is verified on uniform rectangular meshes.
| Original language | English |
|---|---|
| Pages (from-to) | 712-729 |
| Number of pages | 18 |
| Journal | Communications in Computational Physics |
| Volume | 5 |
| Issue number | 2-4 |
| State | Published - Feb 2009 |
| Externally published | Yes |
Keywords
- Artificial compressibility
- Flux difference splitting
- Incompressible Navier-Stokes equations
- Lid-driven cavity flow
- Upwind compact difference
ASJC Scopus subject areas
- Physics and Astronomy (miscellaneous)