| Literature DB >> 34847788 |
P Henningsson1, L C Johansson1.
Abstract
For all flyers, aeroplanes or animals, making banked turns involve a rolling motion which, due to higher induced drag on the outer than the inner wing, results in a yawing torque opposite to the turn. This adverse yaw torque can be counteracted using a tail, but how animals that lack tail, e.g. all insects, handle this problem is not fully understood. Here, we quantify the performance of turning take-off flights in butterflies and find that they use force vectoring during banked turns without fully compensating for adverse yaw. This lowers their turning performance, increasing turn radius, since thrust becomes misaligned with the flight path. The separation of function between downstroke (lift production) and upstroke (thrust production) in our butterflies, in combination with a more pronounced adverse yaw during the upstroke increases the misalignment of the thrust. This may be a cost the butterflies pay for the efficient thrust-generating upstroke clap, but also other insects fail to rectify adverse yaw during escape manoeuvres, suggesting a general feature in functionally two-winged insect flight. When lacking tail and left with costly approaches to counteract adverse yaw, costs of flying with adverse yaw may be outweighed by the benefits of maintaining thrust and flight speed.Entities:
Keywords: aerodynamics; butterflies; flight; manoeuvring
Mesh:
Year: 2021 PMID: 34847788 PMCID: PMC8633796 DOI: 10.1098/rsif.2021.0779
Source DB: PubMed Journal: J R Soc Interface ISSN: 1742-5662 Impact factor: 4.118
Figure 1Kinematic and aerodynamic results from banked turns in silver-washed fritillaries. (a) Bank angle (θ), defined as the angle between a line connecting the wing-tips and the horizon, and yaw angle (φ) as the angle between a line perpendicular to the wing-tip line and the tangent of the horizontally projected path of the turn. Ueff is the flight speed. (b) Bank angle is positively correlated (p < 0.0001) with speed of change of heading () (Blue line: θ = 0.80 (CI ± 0.33) * , r2 = 0.67). For this and the following panels, shaded areas indicate CI of the slope of the fitted lines. (c) Yaw angle was negatively correlated with bank angle (p = 0.024) i.e. showing an uncorrected adverse yaw, but with rather large variation (blue line: φ = –0.46 (CI ± 0.4) * θ –0.72 (CI ± 7.59), r2 = 0.17). (d) We found a positive relation between the yaw angle during the downstroke (φd) and the upstroke (φu) (p < 0.0001) with a stronger adverse yaw during upstroke than during downstroke (blue line: φu = 1.68 (CI ± 0.35) * φd + 0.25 (CI ± 3.62), r2 = 0.75), differing significantly from the predicted 1 : 1 relation (black line). (e) Yaw angle during upstroke correlated well with average side impulse generated during upstroke (Iu) (p < 0.001) (blue line: Iu = 3.62 × 10−7 (CI ± 1.19 × 10−7) * φu – 2.22 × 10−6 (CI ± 2.27 × 10−6), r2 = 0.58), where upstroke impulse acted in the opposite direction to the required centripetal force. (f) Yaw angle during upstroke determines the direction of impulse generated during upstroke (φIu) (p = 0.002) (blue line: φIu = 0.80 (CI ± 0.51) * φu −1.60 (CI ± 12.3), r2 = 0.38), which does not differ from the expected 1 : 1 relation (black line). Regressions are from a mixed linear model taking into account repeated measures within individuals.
Figure 2Vortex wake of a butterfly during a banked turn. The wake, seen from above with flight direction to the left, illustrates variation in yaw angle of the wake between downstroke and upstroke, as indicated by the dashed lines. The upstroke wake indicates force production in the horizontal plane, perpendicular to the dashed line, resulting in thrust and sideways force opposite to the centripetal force required to conduct the turn. Vortices are shown as iso-surfaces of q-criterion coloured by downwash velocity (blue downwards flow and red upwards).