推进技术 ›› 1998, Vol. 19 ›› Issue (4): 78-82.

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基于非交错有限体积格式和 k-ω 湍流模型模拟叶栅湍流分离流动

吴虎,Thiele F   

  1. 西北工业大学航空动力与热力工程系;柏林工业大学HF研究所
  • 发布日期:2021-08-15

NUMERICAL STUDY OF THE CASCADE TURBULENT SEPARATED FLOW BASED ON NON STAGGERED FINITE VOLAME SCHEME AND A k ω TURBULENCE MODEL

  1. Dept.of Aeroengine,Northwestern Polytechnical Univ ,Xi′an,710072;Hermann Fottinger Inst.Technische Univ ,Berlin
  • Published:2021-08-15

摘要: 发展了一种求解任意坐标系下二维N-S方程的非交错有限体积法和一种高阶TVD对流格式。采用一种k-ω湍流模型和几种不同的k-ω模型对叶栅湍流分离流动进行了详细的分析。数值结果与得到的实验结果比较表明,此方法不仅精度高,而且具有较好的数值稳定性。

关键词: 压气机;叶栅流;纳维尔-斯托克斯方程;湍流模型;有限体积法

Abstract: A finite volume numerical method for the solution of two dimensional Navier Stokes equation in general curvilinear coordinates was presented.One or several k ω turbulence models were used to simulate the turbulent flow effects.A non stagered grid system was employed and a specific scheme was presented to suppress the pressure oscillations.A new TVP high order convective differencing scheme was used to improve accuracy and stability in turbulent computations.This method was applied to the turbulent separated flow inside the cascades.The detailed results of computations from different turbulence models were given and the comparisons between numerical results and available experimental data were obtained

Key words: Air compressor;Cascade flow;Navier Stokes equation;Turbulence model;Finite volume method