Improvements in incompressible turbulent horseshoe vortex juncture flow calculations
Abstract
Improvements to a central-difference, finite-volume, explicit Runge-Kutta time-stepping scheme for the steady-state solution of the three-dimensional incompressible, Reynolds-averaged Navier-Stokes equations are presented. Comparisons with the experimental measurements in the turbulent horseshoe vortex flow about an airfoil/flat-plate juncture indicate that both the accuracy and efficiency of the numerical scheme have been improved. In particular, the improved scheme is robust for the problem of high aspect ratio computational cells arising from high Reynolds number flows. A multigrid technique has been implemented to improve the rate of convergence and grid sensitivity has been investigated.
- Publication:
-
29th AIAA Aerospace Sciences Meeting
- Pub Date:
- January 1991
- Bibcode:
- 1991aiaa.meetQS...S
- Keywords:
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- Computational Fluid Dynamics;
- Finite Volume Method;
- Horseshoe Vortices;
- Incompressible Flow;
- Navier-Stokes Equation;
- Turbulent Flow;
- Airfoils;
- Computational Grids;
- Flat Plates;
- High Reynolds Number;
- Runge-Kutta Method;
- Steady State;
- Vorticity;
- Fluid Mechanics and Heat Transfer