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Figure 7


Fig. 7. DPIV results at mid-downstroke (0.25T, the same phase as Fig. 6B). (A) A typical result at 0.29r (effective model wing length r=104 mm). The black thick line denotes wing section and the solid-dot the leading edge. Sectional streamlines are plot. The pseudocolor contour represents the spanwise vorticity. (B) Sectional flow fields at different spanwise locations. The slices were spaced by 15 mm and were all perpendicular to the spanwise direction. Plot representation as in A.





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