中文说明:
NACA0012翼型的网格生成以及零攻角绕流流场计算。
English Description:
Mesh generation and flow field calculation of NACA0012 airfoil at zero angle of attack p>
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中文说明:
NACA0012翼型的网格生成以及零攻角绕流流场计算。
English Description:
Mesh generation and flow field calculation of NACA0012 airfoil at zero angle of attack p>
input.dat
NACA0012.m