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首页> 外文期刊>Journal of Fluids and Structures >Bending-torsional stability analysis of aerodynamically covered pipes with inclined terminal nozzle and concurrent internal and external flows
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Bending-torsional stability analysis of aerodynamically covered pipes with inclined terminal nozzle and concurrent internal and external flows

机译:具有倾斜终端喷嘴的空气动力学覆盖管的弯曲扭转稳定性分析及其内部和外部流动

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Stability analysis of a cantilevered pipe with an inclined terminal nozzle as well as simultaneous internal and external fluid flows is investigated in this study. The pipe is embedded in an aerodynamic cover with negligible mass and stiffness simply to streamline the external flow and avoid vortex induced vibrations. The structure of pipe is modeled as an Euler-Bernoulli beam and effects of internal fluid flow including flow-induced inertia, Coriolis and centrifugal forces and the follower force induced by the exhausting jet are taken into account. In addition, neglecting the compressibility effect and using the unsteady Wagner model, aerodynamic loading is determined as a distributed lateral load for any generic structural state. The integral form of coupled equations of motion are obtained using the Hamilton's principle. Solution to the coupled flexural-torsional equations of motion is realized via the extended Galerkin method. After discretization of the equations of motion, an eigenvalue representation of the problem is obtained. Several parameter studies are then conducted to examine the effects of concurrent fluid flows and other related parameters on the stability margins of the system. (C) 2020 Elsevier Ltd. All rights reserved.
机译:在本研究中研究了倾斜端子喷嘴的悬臂管的稳定性分析以及同时内部和外部流体流动。管道嵌入空气动力学盖中,质量和刚度可忽略不计,简单地简单地简化外部流动并避免涡旋诱导的振动。管道的结构被建模为欧拉-Bernoulli光束,并且内部流体流动的效果包括流动诱导的惯性,科里奥利和离心力,并考虑由排气射流引起的从动射流。另外,忽略压缩效果并使用不稳定的摇头模型,空气动力学载荷被确定为任何通用结构状态的分布式横向载荷。使用Hamilton的原理获得耦合运动方程的整体形式。通过延长的Galerkin方法实现对耦合的弯曲扭转方程的解决方案。在运动方程的离散化之后,获得了问题的特征值表示。然后进行几种参数研究以检查并发流体流动和其他相关参数对系统稳定性边缘的影响。 (c)2020 elestvier有限公司保留所有权利。

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