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

Theodorsen, Theodore Garrick, I E
naca-report-736
1942


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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1942/naca-report-736.pdf