Engineering, 30.05.2020 05:57, kirbymichellrow6zq9

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?

Answers: 1

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

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