Wind-tunnel Investigation of Control-surface Characteristics.: XVI, Pressure Distribution Over an NACA 0009 Airfoil With 0.30-airfoil-chord Beveled-trailing-edge Flaps
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Wind-tunnel Investigation of Control-surface Characteristics.: XVI, Pressure Distribution Over an NACA 0009 Airfoil With 0.30-airfoil-chord Beveled-trailing-edge Flaps