Question: Problem 4 : A wing with span b = 2 0 m has a Gamma distribution given as Gamma ( y ) =

Problem 4:
A wing with span b=20m has a \Gamma distribution given as \Gamma (y)=A *{:(1-((y)/(10))^(4))). In terms of A,
what is the downwash velocity induced by the vortex sheet at the center of the lifting line?
Problem 4 : A wing with span b = 2 0 m has a \

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