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Three-dimensional instabilities in the wake of a flapping wing at low Reynolds number

机译:低雷诺数的机翼拍打后的三维不稳定性

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We present a stability analysis of a plunging and pitching wing of infinite aspect ratio at low Reynolds number. Four cases are considered by varying the mean pitch angle and the phase shift between pitching and plunging. Each case is studied by performing two dimensional DNS and Floquet stability analysis. The four cases considered display different wake structures resulting in different mean aerodynamic forces. Two cases produce thrust and lift, one case only thrust (with symmetric plunging and pitching) and the remaining case mainly lift (with the highest mean pitch angle). In addition, the latter case displays a period doubling phenomenon, and it is found to be linearly unstable for long wavelengths, with an instability mode that resembles that of mode A found in the wake of cylinders. Other cases, although being linearly stable, present a convective instability at smaller wavelengths. Finally, the unstable case has been studied with a fully 3D DNS to evaluate the effect of the three-dimensionality on the forces. The resulting flow structure is consistent with the linear stability analysis in the near wake. Further downstream non-linearities lead to a fully 3D wake. Despite this, the aerodynamic forces on the 3D wing are very similar to those obtained in the 2D simulation. (C) 2016 Elsevier Inc. All rights reserved.
机译:我们提出了在低雷诺数下无限长宽比的俯冲和俯仰机翼的稳定性分析。通过改变平均俯仰角和俯仰与切入之间的相移来考虑四种情况。通过执行二维DNS和Floquet稳定性分析来研究每种情况。所考虑的四种情况显示出不同的尾流结构,导致不同的平均空气动力。有两种情况产生推力和升力,一种情况仅产生推力(对称的俯仰和俯仰),其余的情况主要是升力(具有最大的平均俯仰角)。另外,后一种情况表现出周期加倍现象,并且发现其对于长波长是线性不稳定的,其不稳定模式类似于在圆柱体尾流中发现的模式A。其他情况,尽管是线性稳定的,但在较小的波长下表现出对流不稳定性。最后,已经用完整的3D DNS研究了不稳定情况,以评估三维对力的影响。所得的流动结构与近尾时的线性稳定性分析一致。进一步的下游非线性会导致完全3D唤醒。尽管如此,3D机翼上的空气动力与2D模拟中获得的空气动力非常相似。 (C)2016 Elsevier Inc.保留所有权利。

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