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Unsteady Flowfields Characteristics around Two- and Three-dimensional Flapping Flight

机译:不稳定的流场各种特征在两维和三维扑拍飞行周围

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This paper investigates aerodynamic characteristics of unsteady force generation around two- and three-dimensional flapping motions under forward flight condition. A realistic wing trajectory, called the "figure-of-eight" motion, is extracted from a blowfly's tethered flight under freestream. In order to find out the tendency of vortex generation and flow pattern, two-dimensional simulations are firstly conducted. Computed results show vortical flow fields which exhibit very interesting and distinctive unsteady flowflelds characteristics. Lift is mainly generated during downstroke motion by high effective angle of attack due to translation and lagging motion. On the other hand, a large amount of thrust is generated at the end of upstroke motion. Furthermore, analyses on three-dimensional flapping motions are performed to examine the three-dimensional counterparts of vortex formation and unsteady force generation mechanism. Three—dimensional numerical results show the existence of span-wise vortical flow that prevents the buildup of vorticity separating from the leading edge of the wing, and safely deposits it into a tip vortex. Vortical structure in the wake and the pressure field shows that the vortex pairing and vortex staying mechanism, which are firstly observed in two-dimensional flapping motion, are also observed in three-dimensional flapping motion. Consequently, they can be presented as a strong evidence for the abrupt large thrust generation.
机译:本文研究了在前飞行条件下两维拍打动作周围的不稳定力产生的空气动力学特征。一个逼真的翼轨迹,称为“八件”运动,从FreeStream下的盗版束缚飞行中提取。为了找出涡流产生和流动模式的趋势,首先进行二维模拟。计算结果显示志性流场,展示了非常有趣和独特的非稳定性流量的特征。由于翻译和滞后运动,通过高有效的攻角在下行程运动期间主要产生升力。另一方面,在上行程运动结束时产生大量推力。此外,进行三维拍打运动的分析以检查涡旋形成和不稳定力产生机制的三维对应。三维数值结果表明存在跨越涡流的存在,防止与机翼的前缘分离的涡度的积聚,并将其安全地沉积到尖端涡旋中。在唤醒和压力场中的涡流结构表明,在三维拍摄运动中也观察到涡旋配对和涡旋停留机构首先观察到在二维抖动运动中。因此,它们可以作为突然大推力生成呈现为强大的证据。

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