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Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps. [low turbulence pressure tunnel tests to determine two dimensional lift and pitching moment characteristics

G. J. Bingham, Kevin W. Noonan

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Key concepts: Airfoil, Pitching moment, Chord (peer-to-peer), Turbulence, Wind tunnel, Aerodynamics, Lift (data mining), Mechanics

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Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps. [low turbulence pressure tunnel tests to determine two dimensional lift and pitching moment characteristics — Research Paper | ScholarLens