Page 171 - Introduction to Naval Architecture
P. 171

STRENGTH                           157

        deal with them in any simple way although their effects will be included
        In statistical data recorded at sea if the recorders are sited carefullv.


        STRENGTH OF STRUCTURAL ELEMENTS

        Up to this point it is the overall loading and strength of the hull that has
        been considered. It was pointed out that in deciding which structure to
        include in the section modulus care was necessary to ensure that the
        elements chosen could in fact contribute and would not 'shirk' their
        load. In this section the loading on, and strength of, individual
        elements will be considered.
          The basic structural element is a plate with some form of edge
        support. Combining the plates and their supporting members leads to
        grillages. Bulkheads, decks and shell are built up from grillages. Most of
        the key elements are subject to varying loading so that at times they will
        be in tension and at others in compression. Whilst a structure may be
        more than adequate to take the direct stresses involved, premature
        failure can occur through buckling in compression. This may be
        aggravated by lateral pressure on the plating as occurs in the shell and
        boundaries of tanks containing liquids.
        Buckling
        A structure subject to axial compression will be able to withstand
        loading up to a critical load below which buckling will not occur. Above
        this load a lateral deflection occurs and collapse will eventually follow,
        Euler showed that for an ideally straight column the critical load is:






        where:
            I = column length.
            I - second moment of area of the cross section.
          This formula assumes the ends of the column are pin jointed. The
        critical stress follows as:





        where k is the radius of gyration.
          If the ends of the strut were not pin jointed but prevented from
        rotating, the critical load and stress are increased fourfold. The ratio l/k
        is sometimes called the slenderness ratio. For a strip of plating between
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