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consider a thin airfoil with camber. The camber line is composed of two inverted parabolas with their maxima joined at x=c. Fix the values of...

consider a thin airfoil with camber. The camber line is composed of two inverted parabolas with their maxima joined at x=c. Fix the values of epsilon=0.1 c=1 and plot the lift coefficient, moment coefficient about the leading edge, and the location of the center of pressure for a range of values of alpha and c. show that your answer collapses to the special case of c=c/2.

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