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用RNG K-E模式数值模拟180°弯道内的湍流分离流动

王少平, 曾扬兵, 沈孟育, 中峰, 徐忠

王少平, 曾扬兵, 沈孟育, 中峰, 徐忠. 用RNG K-E模式数值模拟180°弯道内的湍流分离流动[J]. 力学学报, 1996, 28(3): 257-263. DOI: 10.6052/0459-1879-1996-3-1995-329
引用本文: 王少平, 曾扬兵, 沈孟育, 中峰, 徐忠. 用RNG K-E模式数值模拟180°弯道内的湍流分离流动[J]. 力学学报, 1996, 28(3): 257-263. DOI: 10.6052/0459-1879-1996-3-1995-329
NUMERICAL CALCULATION OF TUBULENT SEPARATED FLOWS IN 180 DEG DUCT WITH RNG K ε TUBULENCE MODEL[J]. Chinese Journal of Theoretical and Applied Mechanics, 1996, 28(3): 257-263. DOI: 10.6052/0459-1879-1996-3-1995-329
Citation: NUMERICAL CALCULATION OF TUBULENT SEPARATED FLOWS IN 180 DEG DUCT WITH RNG K ε TUBULENCE MODEL[J]. Chinese Journal of Theoretical and Applied Mechanics, 1996, 28(3): 257-263. DOI: 10.6052/0459-1879-1996-3-1995-329
王少平, 曾扬兵, 沈孟育, 中峰, 徐忠. 用RNG K-E模式数值模拟180°弯道内的湍流分离流动[J]. 力学学报, 1996, 28(3): 257-263. CSTR: 32045.14.0459-1879-1996-3-1995-329
引用本文: 王少平, 曾扬兵, 沈孟育, 中峰, 徐忠. 用RNG K-E模式数值模拟180°弯道内的湍流分离流动[J]. 力学学报, 1996, 28(3): 257-263. CSTR: 32045.14.0459-1879-1996-3-1995-329
NUMERICAL CALCULATION OF TUBULENT SEPARATED FLOWS IN 180 DEG DUCT WITH RNG K ε TUBULENCE MODEL[J]. Chinese Journal of Theoretical and Applied Mechanics, 1996, 28(3): 257-263. CSTR: 32045.14.0459-1879-1996-3-1995-329
Citation: NUMERICAL CALCULATION OF TUBULENT SEPARATED FLOWS IN 180 DEG DUCT WITH RNG K ε TUBULENCE MODEL[J]. Chinese Journal of Theoretical and Applied Mechanics, 1996, 28(3): 257-263. CSTR: 32045.14.0459-1879-1996-3-1995-329

用RNG K-E模式数值模拟180°弯道内的湍流分离流动

NUMERICAL CALCULATION OF TUBULENT SEPARATED FLOWS IN 180 DEG DUCT WITH RNG K ε TUBULENCE MODEL

  • 摘要: 将Yakhot与Orszag新近提出的RNGK-ε湍流模式推广应用于180°强曲率弯道内的湍流分离流动的数值模拟,计算在任意曲线坐标下进行,并采用速度协变分量作为求解变量以保证计算的高度稳定性,控制方程的求解采用通常的控制容积法,文中给出了详细的数值计算结果,并与实验结果进行了比较,结果表明,RNGK-ε湍流模式能有效地模拟有强曲率影响的湍流分离流动,展示了这一模式在工程湍流计算中的前景
    Abstract: A two equation turbulence mode of K ε type was recently derived by Yakhot and Orszag on Renormalization Group (RNG) methods.It was applied to solve the turbulent separated flows in a 180 deg duct.The scheme has been developed for a generalized coordinate system and in based on a control volume approach with a staggered grid arragement.The physical covariant velicity components are selected as the dependent variable in the momentum equations.The detail numerical results were given and compared with th...
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出版历程
  • 刊出日期:  1996-05-24

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