The derivation of Gao-Yong turbulence equations was based on a partial statistical average scheme proposed in the past by the first author in an attempt to capture the drift flow, a first-order statistical moment of turbulent fluctuations. Continuity and momentum equations of turbulent fluctuations were obtained as a result of this valuable first statistical information. Orthotropic turbulence and momentum transfer chain were formulated in the modeling of correlation terms, eventually, led to a complete set of equations of turbu- lent flow with no empirical coefficients and wall functions. Numerical simulations in the past preliminarily veri- fied the adaptability of Gao-Yong equations to a wide range of complex benchmark turbulent flows. In order to further application of these equations to engineering flows, the Gao-Yong turbulence equations were implemen- ted into OpenFOAM and applied to the calculation of wing-body junction flow. The wing-body junction flow in- volves very complex feathers, such as a 3-D separation and a horseshoe vortex. The results of numerical simu- lation of this flow compared to experimental data show that all these main characteristics have been captured, both qualitatively and quantitatively.%Gao—Yong湍流方程基于侧偏统计平均方法保留了湍流脉动量的一阶统计信息，并引入加权漂移速度对称性及正交各向异性，导出漂移流连续方程、动量方程和机械能方程，最后依据湍流物理的唯象论，使用动量传输链概念模化封闭了整个方程组．大量算例验证了此方程对广泛范围的复杂湍流问题的适定性．为了进一步的工程应用，将其加入开源计算流体力学软件OpenFOAM（OpenFieldOperationandManipulation）中，并就翼体角偶流动进行了数值模拟．翼体角偶流动具有三维分离、马蹄涡等十分复杂的流动特征，通过与实验测量结果的对比研究表明，Gao—Yong湍流方程不论在定性还是定量上，都成功捕捉到这类复杂流动现象的主要特征，得到了令人满意的结果．
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