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. 2012 Jan 18;9(72):1674–1684. doi: 10.1098/rsif.2011.0737

Figure 11.

Figure 11.

Four representative cases demonstrating the variation of forces experienced by spread (circle) and non-spread (triangle) tails during a wingbeat cycle. Spread angle Φ pertaining to the maximum force computed for the spread tail is noted. Zones shaded grey correspond to the period of a downstroke.