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. 2019 Jul 10;6(7):190514. doi: 10.1098/rsos.190514

Figure 3.

Figure 3.

Streamlines of the mean velocity field at the quarter plane for a delta wing at α = 0° (a), α = 20° (b) and α = 30° (c) and swift wing at α = 0° (d), α = 20° (e) and α = 30° (f). The red lines highlight streamlines that intersect with the leading edge of the wing.