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Numerical investigation of the aerodynamic benefits of wing-wing interactions in a dragonfly-like flapping wing

机译:龙翼相互作用在蜻蜓型扑翼的空气动力益处的数值研究

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Numerical simulations are performed to investigate the aerodynamic benefits of wing-wing interactions on a dragonfly-like flapping wing while hovering, at a value of Reynolds number Re set to 630. The local phase shift psi and wing spacing L* (L/c) are varied to observe their influence on aerodynamic performance. The results show that the aerodynamic benefits due to interactions are strongly dependent on both psi and L*. The wing-wing interactions are beneficial for the in-phase stroking pattern at psi = 0 degrees when 1.2 <= L* <= 2.3, while it is extremely detrimental for the counter stroking pattern at psi = 180 degrees when 1.2 <= L* <= 2.3; these benefits and drawbacks are dependent on the timing of the interactions. The best case, when psi = 0 degrees and L* = 2.1, can increase the time-averaged vertical force coefficient (C) over bar (v) up to similar to 10 % in comparison to the without-interaction case. Two unsteady flow features namely the enhanced dipole structure and the in-sync of wake capture and wing-wing interactions are observed that increase the vertical force generation in hovering dragonflies. The overall downward momentum imparted by the wing is larger for psi = 0 degrees in comparison to psi = 180 degrees as the wake has high vertical velocities due to the constructive role played by wing-wing interactions.
机译:进行数值模拟以研究蠕动般的泛翼的翼翼相互作用的空气动力学益处,同时悬停在reyynold数重新设置为630.局部移位psi和翼间距l *(l / c)。改变以观察它们对空气动力学性能的影响。结果表明,由于相互作用导致的空气动力学益处强烈依赖于PSI和L *。当1.2 <= L * <= 2.3时,翼翼相互作用对PSI = 0度的同相划分模式有益,而当1.2 <= L *时,在PSI = 180度下对计数器划分模式非常有害。 <= 2.3;这些益处和缺点取决于相互作用的时机。当PSI = 0度和L * = 2.1时,最佳情况下,可以将时间平均垂直力系数(C)增加到与没有相互作用的情况相比相似的杆(V)达到相似的10%。观察到两个不稳定的流量是增强的偶极结构和唤醒捕获和翼翼相互作用的同步,从而增加了悬停蜻蜓中的垂直力产生。由于唤醒具有高垂直速度,PSI = 0度被PSI = 0度赋予PSI = 0度的整体向下动量与由于翼翼相互作用的建设作用,PSI = 180度相比,PSI = 180度相比。

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