Average Lift and thrust variation with phase lag angle (bi-wing).

Table 4: Average Lift and thrust variation with phase lag angle (bi-wing).

Forces		Pitch and Flap phase lag
Forces	0	π/4	π/2	3π/4	π
Average Lift (N)	0.06621198	0.187714154	0.228901395	0.161863869	0.005574254
Average Thrust (N)	0.111028054	0.157128996	0.206268504	0.226252777	0.199126131