\[T = rac{1}{2} ho v^2 C_T A\]
The aerodynamic forces acting on a flapping wing can be described by the following equations:
\[L = rac{1}{2} ho v^2 C_L A\]
\[T = rac{1}{2} ho v^2 C_T A\]
The aerodynamic forces acting on a flapping wing can be described by the following equations:
\[L = rac{1}{2} ho v^2 C_L A\]