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Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60

F E West, T Himka

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Key concepts: Airfoil, Mach number, Lift (data mining), Wing, Compressibility, Lift-to-drag ratio, Structural engineering, Angle of attack

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Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60 — Research Paper | ScholarLens