3 Minutes Using the lift formula, solve for CL, the coefficient of lift. Select the correct equation that is solved for CL. HINT: L=(1/2) D v2 s CL, D=density, v=velocity, s=wing size, L=lift. A) CL=(1/2 D s v2)/L B) CL=(1/2 D)/(s v2 L) C) CL=(1/2 s)/(D v2 L) D) CL=2 L/(D s v2)

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