(Downloading may take up to 30 seconds.
If the slide opens in your browser, select File -> Save As to save it.)
Click on image to view larger version.

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;
, stroke amplitude;
, instantaneous
translational angle. Right: the motion of a section of the wing.
,
instantaneous angle of attack;
, instantaneous rotational angle
(
=90-
°); 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
and
m (maximal rotational angle), respectively. The black line at
t/T=0.25 denotes the DPIV triggering phase.