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Dynamic Response of Wall-Mounted Flaps in an Oscillating Crossflow

机译:振荡横流中壁挂式襟翼的动态响应

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摘要

The coupled interactions between fluids and slender structures play a number of critical roles in a broad range of physical processes. In flow control applications, poroelastic coatings consisting of arrays of passive slender structures have been shown to provide beneficial aerodynamic characteristics when applied to bluff bodies. This effect has been linked to the appearance of a travelling wave through the array which locks in to the shedding frequency of the wake. Through a simplified test case, which reduces the problem complexity while retaining the essential physics of the behaviour, the present work aims to further elucidate this phenomenon via numerical simulations. A range of array lengths are tested and the appearance and propagation of the travelling waves are monitored. The results show that for small arrays there exists one clearly defined wave, which is attributed to the advection of the primary bulk vortex over the array. However, for larger arrays, secondary vortices are generated at the tips which also induce a wave-like behaviour. These secondary vortices are smaller in size and intensity than the primary vortex and induce a smaller deflection in the flaps which dissipates quicker as it propagates though the array.
机译:流体和细长结构之间的耦合相互作用在广泛的物理过程中起多种临界作用。在流量控制应用中,已经示出了由无源细长结构阵列组成的孔隙弹性涂层,以在施加到虚张小体时提供有益的空气动力学特性。这种效果与行波的外观连接到穿过阵列的阵列,该阵列锁定在唤醒的脱落频率上。通过简化的测试用例,这减少了问题复杂性,同时保留了行为的基本物理,目前的作品旨在通过数值模拟进一步阐明这种现象。测试了一系列阵列长度,并监测行驶波的外观和传播。结果表明,对于小阵列,存在一个清晰明确的波,这归因于大量散装涡流在阵列上的平流。然而,对于较大的阵列,在尖端产生次级涡流,这也产生诱导波状行为。这些辅助涡流的尺寸和强度小于主涡流,并且在襟翼中引起较小的偏转,这在诸如阵列传播时更快地消散。

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