Research Article
Trailing Edge Flap Effects on Dynamic Stall Vortex and Unsteady Aerodynamic Forces on a Pitching Airfoil
Figure 25
Comparison of aerodynamic force coefficients for different relative chord lengths of the TEF: (a) lift coefficients, (b) drag coefficients, (c) pitching moment coefficients, and (d) hinge moment coefficients.
(a) |
(b) |
(c) |
(d) |