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Program Foil Edge :

Calculates airfoils coordinates and solves the inviscid potential flow using five different methods

1- Thin airfoil theory , analytical concentrated

2- Lumped vortex panel method , numerical concentrated

3- Constant source + vortex , numerical surface distribution

4- Linear vortex , numerical surface distribution

5- Fifth order partial differential integrator , computational full domain

 

 

 

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