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A Numerical Simulation of Fluid-Structure Interaction for flow through valves of a hermetic compressor with Immersed Boundary Method

机译:具有浸没边界法的气密压缩机流动阀流体结构相互作用的数值模拟

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The aim of the paper is to simulate numerically the Fluid-Structure Interaction for flow through valves of a hermetic compressor using immersed boundary method. The paper is primarily concerned with the mathematical structure and implementation of the Immersed Boundary Method which includes both the Immersed Boundary form of the equations of motion and also the Immersed Boundary numerical Scheme. The flow pattern of the fluid in the compressor is intimately connected with the performance of the valves, and this paper presents a solution of the Navier-Stokes equations in 2D of a Newtonian fluid under laminar regime, in the presence of moving immersed boundaries, being the fluid treated as isothermal. The immersed boundary method has evolved into a generally useful method for problems of Fluid-structure interaction. In this approach, the mathematical formulation employs a mixture of Eulerian and Lagrangian variables, the fluid is represented in a Eulerian co-ordinate frame and the structures or the interacting surfaces are considered in a Lagrangian co-ordinate frame. The two types of variables are linked by interaction equations that involve a smoothed approximation to the Dirac delta function, constructed according to the principles established in [1], which plays a prominent role. In the numerical scheme motivated by the Immersed Boundary formulation, the Eulerian variables are defined on a fixed Cartesian frame, and the Lagrangian variables are defined on a curvilinear mesh that moves freely through the fixed Cartesian mesh without being constrained to adapt to it in any way at all. Eulerian/Lagrangian identities govern the transfer of data from one mesh to another. A structured non-uniform staggered grid based two dimensional finite volume model is used to solve the equations of the fluid flow in laminar regime and a second-order Adams Bashforth-Crank Nicholson scheme is used for temporal discretization and pre-conditioned Bi-conjugate gradient stabilized method is used to solve the derived system of equations. The numerical results presented show the average volumetric flow and the respective temporal valve displacements for different Laminar Reynolds numbers.
机译:纸张的目的是使用浸没边界法在数值上模拟流过气体压缩机的阀的流体结构相互作用。本文主要涉及浸没边界法的数学结构和实施,其包括运动方程的浸没边界形式以及浸没边界数值方案。压缩机中的流体的流动图案与阀门的性能密切相关,本文提出了在移动浸入边界的存在下,在层状制度下的牛顿流体中的2D中的纳米斯斯托克斯方程的解决方案。将流体作为等温。浸没边界法已经发展成流体结构相互作用问题的一般有用的方法。在这种方法中,数学制剂采用欧拉和拉格朗日变量的混合物,流体在欧拉统坐标框架中表示,并且在拉格朗日坐标框架中考虑结构或相互作用表面。这两种类型的变量通过交互方程链接,该交互方程涉及与DIRAC DELTA函数的平滑近似,根据[1]中建立的原理构建,这起到了突出的作用。在由浸没边界配方的数值方案中,欧拉变量在固定的笛卡尔框架上定义,并且拉格朗日变量在曲线网上定义在通过固定的笛卡尔网眼上自由移动而不会被限制以以任何方式适应它根本Eulerian / Lagrangian身份管理将数据从一个网格传输到另一个网格。基于结构化的非均匀交错网格的二维有限体积模型用于解决层流制度中的流体流动的方程,并且二阶ADAMS Bashforth-Crank Nicholson方案用于时间离散化和预调节的双缀合物梯度稳定方法用于解决方程的衍生系统。所示的数值结果显示了不同层状雷诺数的平均体积流量和各个时间瓣膜位移。

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