Engineering, 06.05.2020 02:35 lesly0913

Consider the case where the spanwise circulation distribution ofor a wing is parabolic:
\Gamma (y)= \Gamma _{0}(1-y^{2}/s^{2})
If the total lift generated by the wing with the parabolic circulation distribution is to be equal to the lift generated by a wing with an elliptic circulation distribution,
a) What is the relation between \Gamma _{0} values for the two distributions?
b) What is the relation between the induced downwash velocities at the plane of symmetry for the two configurations?

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Consider the case where the spanwise circulation distribution ofor a wing is parabolic:
\Gamma...

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