Research Article
Computational Investigations on the Effects of Gurney Flap on Airfoil Aerodynamics
Figure 12
Pathlines and turbulence intensities for different positions with 1.5% height GF at AoA = 12°.
(a) Without Gurney flap |
(b) S = 0% |
(c) S = 4% |
(d) S = 10% |