Hello,
NACA 65(2)-415 Airfoil @ 6°AOA, Chord=1,6m (Piper Cherokee)
Could someone please check my simulation for potential mistakes?
My Cl and Cd results seem acceptable.
Is my setup correct?
Especially my meshing and flags.
Did I solve it correctly?
Additionally, any tips or best practices I might have missed would be greatly appreciated.
Thank you in advance for your assistance.
Best regards,
Arne
