Research Article
Trailing Edge Flap Effects on Dynamic Stall Vortex and Unsteady Aerodynamic Forces on a Pitching Airfoil
Table 1
Computational mesh parameters.
| | Parameters | Coarse mesh | Medium mesh | Refined mesh |
| | Nodes on the airfoil | 280 | 550 | 820 | | First layer spacing | c | c | c | | Increasing ratio | 1.12 | 1.10 | 1.08 | | Far-field radius | 100c | 100c | 100c | | Total number of cells | | | |
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