Abstract
A finite volume, cell-centered, density-based flow solver on unstructured grids is developed. The Weiss & Smith precondition matrix is implemented for solving incompressible and compressible flows at all speeds. The AUSMDV (Advection Upstream Splitting Method) scheme with a second order reconstruction is given for the explicit Runge-Kutta and implicit Lower-Upper Symmetric Gauss-Seidel (LU-SGS) time integration methods. Numerical simulation of inviscid flows through a channel with a bump at various Mach numbers and driven flows in a square cavity are presented to demonstrate the performance of the solver. General solution enhancement and convergence acceleration for steady-state Navier-Stokes solutions are attained via the use of inviscid or viscous preconditioning. At last, the analysis of the internal flow in a model solid rocket motor and JPL nozzle are made by the use of this solver. The ability of the solver in providing accurate steady-state solutions for transonic and low-speed flow of variable density fluids is demonstrated.
| Original language | English |
|---|---|
| Pages (from-to) | 89-94 |
| Number of pages | 6 |
| Journal | Engineering Letters |
| Volume | 21 |
| Issue number | 2 |
| State | Published - 21 May 2013 |
Keywords
- All speeds
- Density based
- Flow solver
- Unstructured grids
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