Method for calculating aerodynamic influence coefficients by means of linearized supersonic wing theory; example calculations of influence of flexibility on effectiveness of several lateral control devices and stability derivatives for low aspect ratio configuration.


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    Title :

    Predicted static aeroelastic effects on wings with supersonic leading edges and streamwise tips


    Additional title:

    NASA -- Memo


    Contributors:
    Brown, S.C. (author)


    Publication date :

    1959


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :