主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

新型可压缩尺度在跨声速流动中的应用

Applications of a New Compressible Scale in Transonic Flow

  • 摘要: 基于von Karman长度尺度和新型Reynolds应力本构关系对k-ε湍流模型重构,将k方程封闭,采用代数形式对湍流耗散项进行模化.在KDO(kinetic dependent only)模型的基础上,引入可压缩von Karman长度尺度,得到一种适用于复杂可压缩流动的新型湍流模型CKDO(compressible kinetic dependent only),在CKDO模型中没有任何经验系数,仅有两个来自边界层精细化标定的可调参数.对RAE2822翼型、轴对称圆筒管道凸起流动、ONERA-M6机翼跨声速流动等算例进行数值计算,结果显示CKDO湍流模型对上述算例流场的压力系数模拟结果与实验值吻合较好,表明CKDO模型能够对跨声速流场进行较为准确的模拟.

     

    Abstract: Based on von Karman length scale and new Reynolds stress constitutive relation, the k-equation was closed and the turbulence dissipation term was modeled by algebraic method. On the basis of KDO (kinetic dependent only) model, a compressible von Karman length scale was introduced to obtain a new turbulence model CKDO (compressible kinetic dependent only) for complex compressible flow. There were no empirical coefficients in the CKDO model and only two tunable parameters were derived from the refinement of the boundary layer. The results of the numerical simulations of RAE2822 airfoil, axisymmetric bump pipeline and ONERA-M6 wing transonic flow show that the CKDO turbulence model agrees well with the experimental data for the pressure coefficient simulation of the flow field. It is shown that the CKDO model can simulate the transonic flow field more accurately.

     

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