Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance

Theodorsen, Theodore Garrick, I E

This paper presents a continuation of the work published in Technical Report no. 496. The results of that paper have been extended to include the effect of aerodynamic balance and the effect of a tab added to the aileron. The aerodynamic coefficients are presented in a form convenient for application to the flutter problem.

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