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Fig. 4. Representative flow fields in the wake of the oscillating soft dorsal fin of sunfish during steady swimming at 1.1Ls-1, where L is total body length. AD show wake flow patterns within the frontal-plane laser sheet intersecting the middle of the soft dorsal fin (Fig.2D, position 1) for two consecutive fin half-strokes. The direction of fin motion is indicated by large solid-line arrows. Free-stream velocity (23.1cms-1) from left to right has been subtracted from each velocity vector to reveal vortical wake structures. Schematic illustrations of these structures are given in EH (observed vortices and fluid jets are represented by dashed-line arrows). At this relatively high swimming speed, the soft dorsal fins activity causes substantial deflection and acceleration of the incident flow (cf. Fig.3). (A) As the fin sweeps medially (here at the beginning of a half-stroke), a strong center of vorticity is generated at the fins trailing edge, while opposite-sign vorticity bound to the fin develops upstream. These two rotational flows can be seen converging on the concave surface of the dorsal fin. Note that the jet and clockwise vortex at the right side of this panel were developed during the previous half-stroke in the opposite direction. (B) At the end of the half-stroke, vorticity is released from the trailing edge of the fin and shed into the wake as a free vortex (see counterclockwise flow). Vorticity previously attached to the anterior portion of the fin migrates downstream to contribute to new trailing edge vorticity (clockwise flow). (C) On the return half-stroke, trailing edge vorticity is strengthened and contributes to developing jet flow. (D) By the end of the return stroke, a second vortex has been shed into the wake (see clockwise flow), while opposite-sign, bound vorticity develops at the fins trailing edge. Each complete fin stroke therefore creates a pair of free counterrotating vortices (I and II+III) with a central region of jet flow. Over repeated cycles of soft dorsal fin oscillation, a staggered trail of linked vortices is formed, with downstream jets alternating on the left and right sides of the body. From the momentum of this reverse von Kármán vortex street, stroke-averaged wake forces for propulsion can be calculated. Note that the vortices labeled IIV in EH are directly comparable with those illustrated for turning (see Fig.5F,G). I, starting vortex of half-stroke 1; II, stopping vortex of half-stroke 1; II+III, stopping vortex of half-stroke 1 combined with same-sign starting vortex of half-stroke 2; IV, stopping vortex of half-stroke 2. Scales for AD: arrow, 10cms-1; bar, 1cm.
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