Geometrically exact finite element for thin shells of revolution, using approximation to predict boundary layer stress distribution during vibration


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    Title :

    A geometrically exact finite element for thin shells of revolution.


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING ; 1969 ; NEW YORK, NY


    Publication date :

    1969-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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