Effect of angle of attack and thickness on aerodynamic coefficients of a rigid wing oscillating at very low frequencies in two-dimensional supersonic flow

Frank S. Malvestuto, Jr, Julia M. Goodwin
naca-tn-4069
Jan 1958


Analytical expressions are presented for the lift and pitching-moment coefficients of a wing of finite thickness performing a plunging motion and rotary oscillations about some fixed angle of attack at very low frequencies in two-dimensional flow.

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