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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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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