Cognitive Neurobiology, Department of Biology, Humboldt University , Dorotheenstr.94, 10117 Berlin , Germany ; Present address: Department of Ecology and Evolutionary Biology, Brown University, 34 Olive St, Providence, RI 02912, USA.
Biol Open. 2012 Dec 15;1(12):1226-38. doi: 10.1242/bio.20122964. Epub 2012 Oct 5.
The morphology and kinematics of a flying animal determines the resulting aerodynamic lift through the regulation of the speed of the air moving across the wing, the wing area and the lift coefficient. We studied the detailed three-dimensional wingbeat kinematics of the bat, Leptonycteris yerbabuenae, flying in a wind tunnel over a range of flight speeds (0-7 m/s), to determine how factors affecting the lift production vary across flight speed and within wingbeats. We found that the wing area, the angle of attack and the camber, which are determinants of the lift production, decreased with increasing speed. The camber is controlled by multiple mechanisms along the span, including the deflection of the leg relative to the body, the bending of the fifth digit, the deflection of the leading edge flap and the upward bending of the wing tip. All these measures vary throughout the wing beat suggesting active or aeroelastic control. The downstroke Strouhal number, St(d), is kept relatively constant, suggesting that favorable flow characteristics are maintained during the downstroke, across the range of speeds studied. The St(d) is kept constant through changes in the stroke plane, from a strongly inclined stroke plane at low speeds to a more vertical stroke plane at high speeds. The mean angular velocity of the wing correlates with the aerodynamic performance and shows a minimum at the speed of maximum lift to drag ratio, suggesting a simple way to determine the optimal speed from kinematics alone. Taken together our results show the high degree of adjustments that the bats employ to fine tune the aerodynamics of the wings and the correlation between kinematics and aerodynamic performance.
飞行动物的形态和运动学通过调节流经机翼的空气速度、机翼面积和升力系数来决定产生的空气动力升力。我们研究了蝙蝠(Leptonycteris yerbabuenae)在风洞中飞行时的详细三维翅膀运动学,飞行速度范围为 0-7 m/s,以确定影响升力产生的因素如何在飞行速度范围内和翅膀运动中变化。我们发现,影响升力产生的机翼面积、迎角和拱度随着速度的增加而减小。拱度由沿翼展的多个机制控制,包括腿相对于身体的偏转、第五指的弯曲、前缘襟翼的偏转和翼尖的向上弯曲。所有这些措施在整个翅膀拍打过程中都有所变化,表明存在主动或空气弹性控制。下冲程斯特劳哈尔数(St(d))保持相对恒定,表明在研究的速度范围内,有利的流动特性在下降过程中得以维持。St(d) 通过冲程平面的变化保持不变,从低速时的强烈倾斜冲程平面变为高速时的更垂直冲程平面。翅膀的平均角速度与空气动力性能相关,在最大升力阻力比的速度处达到最小值,这表明仅从运动学就可以确定最佳速度的简单方法。总的来说,我们的研究结果表明蝙蝠采用了高度的调整来微调翅膀的空气动力学,以及运动学和空气动力性能之间的相关性。