Viscous Flow Around An Airfoil - Calculate aerodynamic coefficients using XFoil package | Part 3
In this video we are going to calculate the aerodynamic coefficients of an airfoil at different Reynold's numbers.
First I am going to define an object from the class XFoil and store information about the airfoil geometry created in the previous video.
Then I am going to incorporate the the code into the NACA class in such a way to have a more compact format.
Finally the aerodynamics coefficients in the viscous and invisicid configuarions are calculated at 2 different Reynold's numbers.
All codes are stored in github so feel free to take it and use it as you prefer: https://github.com/FedericoGentile/Ae...
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