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Fig. 3. (A) The wingbeat frequency, f, decreases with increasing flight
speed, U, from 9.1 Hz at 8.0 m s–1 to 8.3 Hz at 9.2
m s–1. (B) Upper (u), lower (d) and total (tot) angular
excursion,
, of the wing in the vertical plane as a function of flight
speed, U. The increase in
tot(U) comes
only from the increase in
u(U). (C) Amplitude,
A, normalized by mean chord length, c. (D) The downstroke
duration, Td, increases with flight speed, U. The
downstroke fraction,
, does not vary with flight speed, U. (E)
The wing angular velocity at mid-upstroke and -downstroke,
,
does not vary greatly with flight speed, U. (F) Wing semispans,
bu,d at mid-upstroke and -downstroke normalized by mean
chord length (c) vs flight speed, U. Wing semispan
does not vary with flightspeed. The span ratio, R, does not change
with flight speed, U. Error bars represent ±s.e.m.