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

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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