Question: he vortex strength distribution, gamma ( x ) , for a thin airfoil at a certain angle of attack is a ) Calculate the

he vortex strength distribution, \gamma (x),for a thin airfoil at a certain angle of attack is
a) Calculate the sectional lift coefficient.
b) Calculate the leading-edge moment coefficient.
c) Determine the center of pressure, xcp
he vortex strength distribution, \ gamma ( x ) ,

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