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

机译:拍打机翼控制飞行力:提升和拖曳生产

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摘要

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. udud(i) For a short, symmetrical wing flip, mean lift was optimized by a stroke amplitude of 180° and an angle of attack of 50°. 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. udud(ii) For a 180° stroke amplitude and a 45° 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. udud(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. udud(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. udud
机译:我们使用果蝇果蝇的动态缩放力学模型来研究机翼运动学的变化如何影响昆虫飞行中不稳定的空气动力的产生。我们检查了191个独立的运动模式集,这些运动模式在笔划幅度,攻角,翻转时间,翻转持续时间以及笔划偏差的形状和大小方面有所不同。使用安装在机翼底部的二维力传感器测量瞬时空气动力。通过将测得力的时间过程与相应的平移准稳态估计的时间过程进行比较,可以评估非稳态旋转效应的影响。对于每种模式,我们还计算了力系数的平均行程平均值,并估算了轮廓功率。该分析的结果可以分为四个要点。 ud ud(i)对于短而对称的机翼翻转,平均升力通过180°的行程幅度和50°的迎角进行了优化。在所有冲程振幅下,平均阻力都随着迎角的增加而单调增加。平移准稳态预测在高行程振幅下比低行程振幅下更好地匹配了测量值。这种差异是由于旋转机构在低冲程幅度的运动学模式中的重要性日益提高。 ud ud(ii)对于180°的行程幅度和45°的迎角,升程通过在行程反转之前稍微发生的短时翻转而最大化。对称旋转产生了类似的高性能。但是,在行程反转后发生的机翼旋转产生的平均升力非常低。 ud ud(iii)空气动力的产生对机翼偏离平均冲程平面的幅度(冲程偏差)的变化以及机翼尖端轨迹的实际形状都非常敏感。然而,在所有示例中,冲程偏差相对于无偏差情况降低了空气动力性能。这种衰减部分是由于升力和总空气动力的径向分量之间的权衡所致。因此,虽然我们没有发现任何证据表明行程偏差会增加升力,但是仍然可以将其用于调节两个机翼上的力。因此,在转向操纵过程中,昆虫可能会利用机翼运动学的这种变化来产生适当的力矩。 ud ud(iv)虽然准稳态估计无法捕获几乎所有运动学模式的测得升程的时程,但它们确实以合理的精度预测了平均升程系数的行程平均值。但是,准稳态估计严重低估了所有条件下的平均阻力系数的大小。这种差异是由于稳态估计无法捕捉到的旋转效应所致。该结果表明,许多先前基于机翼运动学的机械功率估计可能被严重低估了。 ud ud

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  • 年度 2001
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  • 正文语种 {"code":"en","name":"English","id":9}
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