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A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

Edward C B Danforth

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Key concepts: Airfoil, NACA airfoil, Transonic, Lift-to-drag ratio, Angle of attack, Mathematics, Series (stratigraphy), Drag coefficient

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A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio — Research Paper | ScholarLens