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A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution

David Graham

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Key concepts: Airfoil, Lift (data mining), Section (typography), Mechanics, Geometry, Lift-to-drag ratio, Lift coefficient, Mathematics

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A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution — Research Paper | ScholarLens