*The aerofoil profile coordinates data  imported from online library(Airfoiltools.com)
*The Ansys Design modular(academic version) is used to create geometry
*The Ansys Fluent(Academic version) meshing is used as meshing tool


#comment out the line in velocity(U) file of 0 diectory to change angle of attack.

#TO convert fluent mesh to foam mesh use the command  "fluentMeshToFoam naca2415.msh" (this will generate polymesh mesh folder ).


#To run the simulation use command "./Allrun" (""The Allrun command already set  with fluent to foam mesh conversion so no need of  
use fluentmeshtofoam at first"")


#To view countors and plots in paraview use command  "paraFoam"


