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Nonlinear dynamic responses of a perimeter-reinforced membrane wing in laminar flows

机译:层流钢流动膜翼的非线性动力响应

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摘要

Dynamic responses of a two-dimensional (2D) perimeter-reinforced (PR) membrane wing in laminar viscous flows are investigated numerically. The 2D Navier-Stokes equations and a one-dimensional nonlinear equation for membrane vibration are coupled to describe the flow-induced vibrations of the membrane wing in laminar flows. The modified characteristic-based split scheme, Galerkin finite element method, spring analogy technique and loosely coupled partitioned approach are employed, respectively, for the flow simulation, computation of the membrane response, mesh movement of the flow domain and fluid-structure interaction. The accuracy and stability of the proposed numerical method and corresponding codes are validated using a benchmark model of fluid-membrane interaction. Finally, the bifurcation characteristics of the membrane dynamic response and vortex structure near the membrane wing with respect to the angle of attack, Reynolds number, rigidity and pre-strain are analysed in detail. This paper could give people more information about the dynamic behaviours of the PR membrane wing in the laminar flow regime.
机译:在数值上研究了层状粘性流动中的二维(2D)周边增强(Pr)膜翼的动态响应。 2D Navier-Stokes方程和用于膜振动的一维非线性方程耦合以描述层流中膜翼的流动诱导的振动。分别采用了改进的特征的分流方案,Galerkin有限元方法,弹簧模拟技术和松散耦合的分隔方法,用于流动模拟,膜响应的计算,流动域的网格运动和流体结构相互作用。使用流体 - 膜相互作用的基准模型验证了所提出的数值方法和相应码的精度和稳定性。最后,详细分析了膜翼膜翼型近膜机翼附近的膜动力响应和涡旋结构的分岔特性,详细分析了雷诺数,刚性和预菌株。本文可以提供有关Laminar流程中Pr膜翼的动态行为的更多信息。

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