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The NUmerical Osciliations Caused by the Boundaries Treatments in the Solution of the Euler Quasi-One-Dimensional Model

机译:欧拉拟一维模型解中边界处理引起的数值振荡

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This paper deals with the numerical oscillations in the solution of the compressible, unsteady and quasi-one-dimensional model of Euler governing the subsonic flow inside a portion of a duct with non-physical boundaries. The presence of these oscillations is particularly obvious in the solution of a real flow where the boundary conditions are taken by measurements in an intake apparatus of a reciprocating engine. No absorbent boundary treatment is allowed because a time dependent solution is searched. Each boundary could be considered as an acoustical source. The resolution is done with the finite difference schemes of Lax-Wendroff or Harten-Roe (TVD). The diagnostic is done by observing the numerical resolution of a progressive acoustical pulsation in a subsonic steady flow whose analytical solution is known as been the solution of the equation of Pridmore-Brown. We explain how these oscillations take place at the entrance boundary and the roles of the resolution scheme and the scheme of establishment of the numerical boundary conditions. The physical boundary condition at the exit induce the trapping of the residual waves at the origin of these oscillations. The behavior of these ones is also interpreted. We also explain the presence of an entropic perturbation in the solution.
机译:本文讨论了可压缩,不稳定和准一维欧拉模型的解中的数值振荡,该模型控制着具有非物理边界的部分管道内的亚音速流。这些振荡的存在在实际流动的解决方案中特别明显,在实际流动中,边界条件是通过在往复式发动机的进气装置中进行测量来获取的。不允许进行吸收剂边界处理,因为要搜索与时间有关的解决方案。每个边界都可以看作是声源。分辨率是通过Lax-Wendroff或Harten-Roe(TVD)的有限差分方案完成的。通过观察亚音速稳定流中渐进声波脉动的数值分辨率来完成诊断,其解析解被称为Pridmore-Brown方程的解。我们将解释这些振荡如何在入口边界处发生,以及解析方案和数值边界条件建立方案的作用。出口处的物理边界条件导致残留波在这些振荡的起点处被捕获。这些行为也会被解释。我们还解释了溶液中存在熵扰动。

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