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通过扑翼对飞行力的控制:升力和阻力的产生。

The control of flight force by a flapping wing: lift and drag production.

作者信息

Sane S P, Dickinson M H

机构信息

Department of Integrative Biology, University of California, Berkeley, CA 94720, USA.

出版信息

J Exp Biol. 2001 Aug;204(Pt 15):2607-26. doi: 10.1242/jeb.204.15.2607.

Abstract

We used a dynamically scaled mechanical model of the fruit fly Drosophila melanogaster to study how changes in wing kinematics influence the production of unsteady aerodynamic forces in insect flight. We examined 191 separate sets of kinematic patterns that differed with respect to stroke amplitude, angle of attack, flip timing, flip duration and the shape and magnitude of stroke deviation. Instantaneous aerodynamic forces were measured using a two-dimensional force sensor mounted at the base of the wing. The influence of unsteady rotational effects was assessed by comparing the time course of measured forces with that of corresponding translational quasi-steady estimates. For each pattern, we also calculated mean stroke-averaged values of the force coefficients and an estimate of profile power. The results of this analysis may be divided into four main points. (i) For a short, symmetrical wing flip, mean lift was optimized by a stroke amplitude of 180 degrees and an angle of attack of 50 degrees. At all stroke amplitudes, mean drag increased monotonically with increasing angle of attack. Translational quasi-steady predictions better matched the measured values at high stroke amplitude than at low stroke amplitude. This discrepancy was due to the increasing importance of rotational mechanisms in kinematic patterns with low stroke amplitude. (ii) For a 180 degrees stroke amplitude and a 45 degrees angle of attack, lift was maximized by short-duration flips occurring just slightly in advance of stroke reversal. Symmetrical rotations produced similarly high performance. Wing rotation that occurred after stroke reversal, however, produced very low mean lift. (iii) The production of aerodynamic forces was sensitive to changes in the magnitude of the wing's deviation from the mean stroke plane (stroke deviation) as well as to the actual shape of the wing tip trajectory. However, in all examples, stroke deviation lowered aerodynamic performance relative to the no deviation case. This attenuation was due, in part, to a trade-off between lift and a radially directed component of total aerodynamic force. Thus, while we found no evidence that stroke deviation can augment lift, it nevertheless may be used to modulate forces on the two wings. Thus, insects might use such changes in wing kinematics during steering maneuvers to generate appropriate force moments. (iv) While quasi-steady estimates failed to capture the time course of measured lift for nearly all kinematic patterns, they did predict with reasonable accuracy stroke-averaged values for the mean lift coefficient. However, quasi-steady estimates grossly underestimated the magnitude of the mean drag coefficient under all conditions. This discrepancy was due to the contribution of rotational effects that steady-state estimates do not capture. This result suggests that many prior estimates of mechanical power based on wing kinematics may have been grossly underestimated.

摘要

我们使用了果蝇黑腹果蝇的动态缩放力学模型,来研究翅膀运动学的变化如何影响昆虫飞行中不稳定气动力的产生。我们研究了191组不同的运动学模式,这些模式在冲程幅度、攻角、翻转时间、翻转持续时间以及冲程偏差的形状和大小方面存在差异。使用安装在翅膀基部的二维力传感器测量瞬时气动力。通过将测量力的时间历程与相应的平移准稳态估计值进行比较,评估不稳定旋转效应的影响。对于每种模式,我们还计算了力系数的平均冲程平均值和轮廓功率的估计值。该分析结果可分为四个要点。(i) 对于短而对称的翅膀翻转,平均升力在冲程幅度为180度、攻角为50度时达到最佳。在所有冲程幅度下,平均阻力随着攻角的增加而单调增加。在高冲程幅度下,平移准稳态预测比在低冲程幅度下更能匹配测量值。这种差异是由于在低冲程幅度的运动学模式中旋转机制的重要性增加。(ii) 对于180度的冲程幅度和45度的攻角,在冲程反转前稍早发生的短持续时间翻转可使升力最大化。对称旋转产生类似的高性能。然而,在冲程反转后发生的翅膀旋转产生的平均升力非常低。(iii) 气动力的产生对翅膀偏离平均冲程平面的幅度(冲程偏差)变化以及翼尖轨迹的实际形状敏感。然而,在所有示例中,冲程偏差相对于无偏差情况降低了气动力性能。这种衰减部分是由于升力与总气动力的径向分量之间的权衡。因此,虽然我们没有发现冲程偏差可以增加升力的证据,但它仍然可以用于调节两个翅膀上的力。因此,昆虫在转向机动过程中可能会利用翅膀运动学的这种变化来产生适当的力矩。(iv) 虽然准稳态估计几乎无法捕捉到几乎所有运动学模式下测量升力的时间历程,但它们确实以合理的精度预测了平均升力系数的冲程平均值。然而,准稳态估计在所有条件下都严重低估了平均阻力系数的大小。这种差异是由于稳态估计未捕捉到的旋转效应的贡献。这一结果表明,许多先前基于翅膀运动学的机械功率估计可能被严重低估了。

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