The lift force affecting the airfoil is the incoming flow velocity V and density , chord length
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The lift force affecting the airfoil is the incoming flow velocity V∞ and density ρ∞, chord length b, sound velocity a∞, thickness C, curvature f , angle of attack α, sideslip angle β, and gravitational acceleration g. Please use the dimensional analysis method to give the dimensionless expression of the lift coefficient.
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