Euler
代码说明:
基于James格式的CFD程序,计算NACA0012翼型流场和升力阻力系数.网格由Fluent提供的Gmbit生成,计算结果可以通过Tecplot观看(James formats based on the CFD program to calculate the flow field and the NACA0012 airfoil lift drag coefficient. Fluent grid provided by the Gmbit generated, calculated results can Tecplot Views)
文件列表:
Euler
.....\Debug
.....\Euler.cpp
.....\Euler.dsp
.....\Euler.dsw
.....\Euler.ncb
.....\Euler.opt
.....\Euler.plg
.....\Euler2.cpp
.....\NACA0012.msh
.....\pre_mesh.cpp
.....\ReadMe.txt
.....\StdAfx.cpp
.....\StdAfx.h
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