Title: Effect of Angle of Attack and Thickness on Aerodynamic Coefficients of a Rigid Wing Oscillating at Very Low Frequencies in Two-dimensional Supersonic Flow
Abstract: Report presenting an analytical expression 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. Calculated lift and pitching-moment coefficients and design charts are presented.
Publication Year: 1958
Publication Date: 1958-01-01
Language: en
Type: article
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