使用GAO-YONG方程组对可压湍流边界层的数值模拟
The Calculation of Wall Boundary Layer Using GAO-YONG Turbulence Equations
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摘要: 应用SIMPLE/SIMPLER方法及QUICK格式求解GAO-YONG可压湍流方程组,对二维零压力梯度可压平板湍流边界层进行了数值模拟。结果表明,不需要任何经验系数及壁面函数的GAO-YONG可压湍流控制方程组对较广马赫数范围(Ma=0.2~2.4)平板边界层各项参数(表面摩擦系数Cf,对数律,亏损律等)能做出良好的预测。
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关键词:
- 航空、航天推进系统 /
- 湍流 /
- GAO-YONG理性湍流方程 /
- 可压湍流边界层
Abstract: Two-dimensional,stationary,compressible boundary layer with zero pressure gradient is numerically simulated with GAO-YONG turbulence model.Employing staggered grid arrangement,SIMPLE/SIMPLER code and a second-order QUICK scheme are used.All the results verify that the GAO-YONG equations,without using empirical coefficients and wall functions,may successfully simulate the compressible turbulent boundary layer (Ma=0.2~2.4).The calculation successfully simulates the flow,including the natural transition process,and predicts the fundamental properties of the boundary layer,such as C_f,the logarithmic law, and the defect law,etc,which are finely close to the experimental data.All the results further verify the adaptability of the turbulence model to real turbulent flow.
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