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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    01.01.1942


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Nonstationary flow about Wing-Aileron-Tab combination including aerodynamic balance

    Theodorsen, T. / Garrick, I.E. | Engineering Index Backfile | 1942



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