Complexity of the phenomena of panel flutter instability has resulted in the necessity of developing separate design criteria for a variety of flow conditions and panel configurations. Vehicle panel configurations with low aspect ratios are of interest in low supersonic flow, where boundary layer effects are important.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic forces of fluttering cylindrical and/or planar structures


    Contributors:

    Publication date :

    1969-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Fluttering fountains

    Casperson, L.W. | Online Contents | 1993



    Minitype fluttering-wing aircraft

    WANG ZHICHENG | European Patent Office | 2015

    Free access