文件1.f90：生成翼型naca0012的椭圆网格，并计算流场，给出壁面压力分布 文件2.f90：maccormack方法解一维burger s方程 文件3.f90：解一维laval管流动，其进出口均为亚音速，喉道后部有激波-File 1.f90: generate the airfoil naca0012 elliptical rotary cell, and calculate the flow field, given the wall pressure distributio

NACA0012翼型O网格生成；速度势方程解流场-NACA0012 airfoil O mesh generation flow field velocity potential equation

用来生成翼型NACA0012的计算网格，此网格可用于后续计算。程序数据在附件里。(A computational mesh used to generate airfoil NACA0012)

NACA0012翼型的网格生成以及零攻角绕流流场计算(Mesh generation of NACA0012 airfoil and calculation of flow field around zero angle of attack)