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      THE EFFECT OF A CAVITY ON PANEL VIBRATION

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      AIAA Journal
      American Institute of Aeronautics and Astronautics (AIAA)

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          The Buckling of Thin Cylindrical Shells Under Axial Compression

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            Author and article information

            Journal
            AIAA Journal
            AIAA Journal
            American Institute of Aeronautics and Astronautics (AIAA)
            0001-1452
            1533-385X
            February 1963
            February 1963
            : 1
            : 2
            : 476-477
            Article
            10.2514/3.1568
            eea8a1fe-3dfb-4ad8-8815-d28769af5b60
            © 1963
            History

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