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Not so long ago, we had #140 solving bugs regarding airfoil implementation.
It's true that now rocketpy is dealing very well with these non-flat fins, however I feel we could implement some plots in rocket.py file to show to the user.
Some of them could be:
- Simple plot of airfoil data the user inputed by addFins() method
- Derivative of Lift coefficient by angle of attack
But of course feel free to add any other information you consider important!
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Good first issueGood for newcomersGood for newcomers