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ROUTINES FOR GENERATION OF A C-TYPE GRID SYSTEM USE FOR FLOWS PAST AN AIRFOIL
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采用偏微分方程数值解法生成翼型O型网格并采用速度势方程求低速不可压无粘流场 -Numerical solution of partial differential equations using Airfoil O-grid generation and use low-speed velocity potential Equation incompressible inviscid flow field
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This Fortran Program develop for NACA0200 Airfoil Axi-symmetric grid generation. The grid is clustered in x. Program is basic level for under graduate students.
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偏微分方程法生成翼型C网格程序 fortran-PDE grid generation method program fortran airfoil C
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绕翼型网格生成程序，采用O型网格，拉普拉斯方程。-Around the airfoil mesh generation process, the use of O-type grid, Laplace s equation.
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This Project Includs Various Kinds of Grid Generation Around a NACA0012 Airfoil
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structured grid generation around airfoil NACA 4 digits
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unstructured grid generation around airfoil
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This Fortran Program develop for NACA0200 Airfoil Axi-symmetric grid generation. The grid is clustered in x. Program is basic level for under graduate students.
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基于椭圆型偏微分方程生成二维NACA0012翼型的O型网格并求解流场(Generation of O-grid of two-dimensional NACA0012 airfoil and solution of flow field based on elliptic partial differential equation)
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