(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. 2. Definition of the diameter and angle relative to the horizon of the vortex
ring generated at the outer wing during the end of the upstroke (see text) as
seen in the streamwise [x–z] (A) and transverse
[y–z] (B) planes. The small vortices (small orange-
and blue-filled circles) represent the outer wing vortex ring. The large
circles represent start (orange) and stop (blue) in A and mid-wing vortices in
B. The inserted wake models of the near wake at a flight speed of 4 m
s–1, as suggested previously
(Hedenström et al.,
2007), show the laser sheet cut through the wake. Blue
cross-stream tubes represent start vorticity and red cross-stream tubes stop
vorticity. Blue streamwise tubes represent tip vortices and red streamwise
tubes root vortices. At the end of the upstroke the outer wing sheds separate
vortex rings, shown in dark red.