Research Article
Computational Investigations on the Effects of Gurney Flap on Airfoil Aerodynamics
Figure 8
Pathlines and turbulence intensities for different GF heights at AoA = 10°.
| (a) Without Gurney flap |
| (b) H = 1% |
| (c) H = 2% |
| (d) H = 3% |
| (a) Without Gurney flap |
| (b) H = 1% |
| (c) H = 2% |
| (d) H = 3% |