1.

Select the incorrect equation for the induced drag coefficient for a finite wing.

A. C<sub>D,i</sub>= ( frac {C_l^2}{ pi AR} )(1+ )
B. C<sub>D,i</sub>= ( frac {C_l^2}{ pi AR} )
C. C<sub>D,i</sub>= ( frac {C_l^2s}{ pi eb^2 } )
D. C<sub>D,i</sub>= ( frac {C_l^2}{ pi eAR} )
Answer» C. C<sub>D,i</sub>= ( frac {C_l^2s}{ pi eb^2 } )


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