A numerical procedure was developed for minimizing the structural mass of an aircraft structure which must have a specified minimum flutter velocity or divergence velocity. During the optimization process the arrangement of the structural members remains fixed, while the stiffness parameters of the structure are varied.


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    Title :

    Optimization of fiber reinforced structures to satisfy aeroelastic requirements


    Contributors:

    Publication date :

    1981-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English