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Figure 3


Fig. 3. Sketch of flapping motion in hovering. (A) Left: spatial configuration of the flapping motion of a model wing. The thick black line denotes the leading edge; OT, translational axis; OZ, rotational axis; OD and OU, the translational extreme positions; R, model wing length; r, effective model wing length; {Phi}, stroke amplitude; {varphi}, instantaneous translational angle. Right: the motion of a section of the wing. {alpha}, instantaneous angle of attack; {rho}, instantaneous rotational angle ({rho}=90-{alpha}°); black thick line denotes wing section and solid-dot, the leading edge. (B) The kinematic curves over one period. The translational and rotational angular positions are normalized using {Phi} and {rho}m (maximal rotational angle), respectively. The black line at t/T=0.25 denotes the DPIV triggering phase.





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