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.
Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance
1942-01-01
Miscellaneous
No indication
English
Nonstationary flow about Wing-Aileron-Tab combination including aerodynamic balance
Engineering Index Backfile | 1942
|Engineering Index Backfile | 1954
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