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arXiv 2011.11422physics.flu-dyn

中等雷诺数下流动激发的薄膜不稳定性

Flow-excited membrane instability at moderate Reynolds numbers

Guojun Li, Rajeev Kumar Jaiman, Boo Cheong Khoo

AI总结:

本文通过高保真数值模拟研究中等雷诺数下三维柔性薄膜的流动激发不稳定性,发现涡脱落频率与薄膜固有频率的锁定导致自持振动,并提出了稳定性相图,为薄膜机翼无人机控制策略设计提供依据。

摘要:

本文研究了一个三维(3D)柔性薄膜浸没在中等雷诺数非定常分离流中的流体-结构相互作用(FSI)。我们采用基于最近发展的分区迭代格式的体协调变分FSI求解器,用于耦合湍流流体流动与非线性结构动力学。特别关注的是理解三维柔性薄膜的流动激发不稳定性,作为无量纲质量比、雷诺数和气动弹性数的函数。在广泛的参数范围内,我们考察了流体-薄膜相互作用的两种不同稳定状态:变形稳态(DSS)和动态平衡态(DBS)。我们提出了稳定性相图,以在质量比与雷诺数以及质量比与气动弹性数的参数空间中划分DSS和DBS区域。基于气动弹性模态分析,我们观察到涡脱落频率与薄膜振动频率之间的频率同步,这导致了动态平衡态中的自持振动。为了表征频率锁定的起源,我们通过考虑附加质量效应并采用简支矩形薄膜的大挠度理论,推导了非线性固有频率的近似解析公式。通过我们系统的高保真数值研究,我们发现薄膜振动的起始和模态转变依赖于张紧薄膜的固有频率与涡脱落频率或其谐波之间的频率锁定。这些关于薄膜流体弹性不稳定性的发现,对基于薄膜机翼的无人系统和无人机的控制策略的设计和开发具有启示意义。

英文摘要:

In this paper, we study the fluid-structure interaction (FSI) of a three-dimensional (3D) flexible membrane immersed in an unsteady separated flow at moderate Reynolds numbers. We employ a body-conforming variational FSI solver based on the recently developed partitioned iterative scheme for the coupling of turbulent fluid flow with nonlinear structural dynamics. Of particular interest is to understand the flow-excited instability of a 3D flexible membrane as a function of the non-dimensional mass ratio, Reynolds number and aeroelastic number. For a wide range of the parameters, we examine two distinctive stability regimes of fluid-membrane interaction: deformed-steady state (DSS) and dynamic balance state (DBS). We propose stability phase diagrams to demarcate the DSS and DBS regimes for the parameter space of mass ratio vs. Reynolds number and mass ratio vs. aeroelastic number. Based on the aeroelastic mode analysis, we observe a frequency synchronization between the vortex shedding frequency and the membrane vibration frequency which leads to self-sustained vibrations in the dynamic balance state. To characterize the origin of the frequency lock-in, we derive an approximate analytical formula for the nonlinear natural frequency by considering the added mass effect and employing a large deflection theory for a simply supported rectangular membrane. Through our systematic high-fidelity numerical investigation, we find that the onset of the membrane vibration and the mode transition has a dependence on the frequency lock-in between the natural frequency of the tensioned membrane and the vortex shedding frequency or its harmonics. These findings on the fluid-elastic instability of membranes have implications for the design and development of control strategies for membrane wing-based unmanned systems and drones.

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