Theory of static aeroelastic stability of supersonic wings including chordwise bending, as previously developed, is further extended to include influence of stresses arising from thermal gradients.


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    Title :

    Influence of thermal stresses on aeroelastic stability of supersonic wings


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Biot, M.A. (author)


    Publication date :

    1957


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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