Research Article
Trailing Edge Flap Effects on Dynamic Stall Vortex and Unsteady Aerodynamic Forces on a Pitching Airfoil
Figure 27
Comparison of aerodynamic force coefficients at different minimum deflection angles of the TEF: (a) lift coefficients, (b) drag coefficients, (c) pitching moment coefficients, and (d) hinge moment coefficients.
| (a) |
| (b) |
| (c) |
| (d) |