Theory of divergence of constant thickness rectangular plate wings is presented, based on assumptions of linear elastic theory and linearized aerodynamic theory; critical conditions occurred at M equal 1; it is established that sweeping leading edge of plate airfoil of constant thickness increases its stability; divergence conditions.


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    Title :

    Divergence of plate airfoils of low aspect ratio at supersonic speeds


    Additional title:

    J Aero/Space Sciences


    Contributors:

    Published in:

    Publication date :

    1959


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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