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Problem 4 (10 points). Consider the case where the spanwise circulation distribution for a wing is parabolic, Γ(y) = Γο.
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Problem 4 (10 points). Consider the case where the spanwise circulation distribution for a wing is parabolic, Γ(y) = Γο.
Problem 4 (10 points). Consider the case where the spanwise circulation distribution for a wing is parabolic, Γ(y) = Γο. 0_Parab 4y? b2 dw If the total lift generated by the wing with the parabolic circulation distribution is to be equal to the total lift generated by a wing with an elliptic circulation distribution, dy dr V. Lifting line Γ(y) = Γο_Ellie 4y? what is the relation between the values of To_Parab and To_Ellip for the two distributions?
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