Triangular panel method predicting lift curve slope more than thin airfoil theory

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Aaditya Wangikar asked 10 months ago

For the wing I have geometric and aerodynamic twist at different sections. I am getting lift curve slope more than 2*pi, which is more than thin airfoil theory. What could be the possible reasons??

techwinder Staff replied 10 months ago

Unfortunately, I don’t know.

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