An experimental setup is prepared in order to evaluate the effects of wing flexibility on lift, thrust and power loading of the flapping wings with bending deflection angle (B.D.A.). Hence, two wings with different ...

The main objective of this research is to evaluate the effects of the wing bending deflection angle (B.D.A) on thrust force for different flapping frequencies at 10 degree angles of attack (AOA) in hovering flight. Moreover, ...