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. 2010 Dec 3;8(59):807–816. doi: 10.1098/rsif.2010.0533

Figure 2.

Figure 2.

Illustration showing how the angle (β) of the wake plane was measured and used to derive instantaneous vertical force (lift, L) and horizontal force (thrust/drag, T/D) from the total instantaneous force (Finst). The bird is flying form left to right and the two grey trails symbolizes the wingtip vortices left behind in the wake.