Continuation of work published in Report No. 496 indexed in Engineering Index 1935 p 19, under heading Airplane Control Surfaces -- Flutter; results of that paper have been extended to include effect of aerodynamic balance and effect of tab added to aileron; aerodynamic coefficients presented in form convenient for application to flutter problem.


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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1942


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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