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Computational fluid dynamic modeling of cavitating flows.

机译:空化流的计算流体动力学建模。

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摘要

Sheet cavitation on hydrofoils is analyzed in Euler and Navier-Stokes codes using a model analogous to velocity potential theories. The approach taken is to ensure compatibility with previous velocity potential models before implementing this model in Euler and Navier-Stokes codes. The Navier-Stokes model is augmented by the inclusion of the energy equation which allows modeling of the effect subcooling in the vicinity of the cavity interface to take into account the thermodynamic effects of cavitation in cryogenic fluids. Both a fully nonlinear and a linearized model are developed. In both models, the cavity length and inception point evolve as part of the solution. The nonlinear model uses the cavity surface as a streamline, so that the numerical grid must evolve with the solution. The linearized model uses the initial surface grid throughout the solution and enforces approximate boundary conditions on the airfoil surface in a linearized airfoil fashion to force the streamlines to divert around the cavitation bubble. The cavitation models developed provide extension to more complex geometries and flows than can be addressed by velocity potential models.; The primary emphasis in this thesis centers on two-dimensional computations. The generality of the formulation in the Euler and Navier-Stokes codes allows for representative three-dimensional calculations to be presented. Comparisons between velocity potential, Euler and Navier-Stokes implementations indicate they all produce fairly consistent predictions. Comparisons with experimental measurements also indicate that the predictions are qualitatively correct and give a reasonable first estimate of sheet cavitation effects for both cryogenic and non-cryogenic fluids. The three-dimensional calculations demonstrate the extension of the model to more complex flows. The added computational resources required by the cavitation model are minimal, as are the code modifications required to implement the model, indicating that these models are appropriate for incorporation in current generation turbomachinery codes for engineering predictions of sheet cavitation effects.
机译:使用类似于速度势理论的模型,以Euler和Navier-Stokes代码分析水翼上的气蚀现象。采取的方法是在用Euler和Navier-Stokes代码实现该模型之前,确保与以前的速度势模型兼容。通过包含能量方程式来扩展Navier-Stokes模型,该方程式允许对腔体界面附近的过冷效应建模,以考虑到低温流体中的空化效应。开发了完全非线性模型和线性模型。在这两个模型中,型腔的长度和起始点都是解决方案的一部分。非线性模型使用型腔表面作为流线,因此数值网格必须随解而演化。线性化模型在整个解决方案中使用初始表面网格,并以线性化翼型方式在翼型表面上施加近似边界条件,以迫使流线围绕空化气泡转移。开发的空化模型提供了比速度势模型无法解决的更复杂的几何形状和流动。本文的主要重点是二维计算。 Euler和Navier-Stokes代码中公式的一般性允许呈现代表性的三维计算。速度势,Euler和Navier-Stokes实现之间的比较表明,它们都产生了相当一致的预测。与实验测量值的比较还表明,该预测在质量上是正确的,并且给出了低温和非低温流体的薄板空化效应的合理的第一估计。三维计算证明了模型的扩展到更复杂的流。空化模型所需的附加计算资源最少,实现该模型所需的代码修改也很少,这表明这些模型适用于并入当前的涡轮机械代码中,以进行薄片空化效果的工程预测。

著录项

  • 作者

    Deshpande, Manish.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1995
  • 页码 215 p.
  • 总页数 215
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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