首页> 外文会议>International Conference on Computational Fluid Dynamics(ICCFD3); 20040712-16; Toronto(CA) >Numerical Study on k-ω Turbulence Models for Supersonic Impinging Jet Flow Field
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Numerical Study on k-ω Turbulence Models for Supersonic Impinging Jet Flow Field

机译:超音速撞击射流场的k-ω湍流模型的数值研究

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摘要

The result of a computational investigation for an underexpanded jet and impingement on a wall with various distances from the jet exit is presented. The three-dimensional Navier-Stokes equations and a number of two-equation turbulence models based on the ω equation are computed. It is shown that the pressures on the impinging plate with the weakly nonlinear eddy viscosity model is in good agreement with the experimental data, particularly, in the case of occurrence of the stagnation bubble.
机译:给出了计算不足的射流和撞击到距射流出口各种距离的墙壁的计算结果。计算了三维Navier-Stokes方程和基于ω方程的多个二方程湍流模型。结果表明,涡流模型为弱非线性时,冲击板上的压力与实验数据吻合较好,特别是在出现滞流气泡的情况下。

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