Numerical investigation of three - dimensional steady jet - interaction phenomenology . ( 1 ) aerodynamics characteristic is calculated by using renolds - averaged navier - stokes equations discretitted in cell - centered finite volume framework and improved on baldwin - lomax turbulent model for the slender body at the high angle of attack ( 1 )采用三维积分形式n - s方程的中心有限体积离散方法，提出了改进的b - l湍流模型，进行了较大攻角弹体的气动特性计算和结果分析。
