Page 161 - Introduction to Naval Architecture
P. 161

STRENGTH                          147

        M is a distribution factor along the length. It is taken as unity between
        0.4L and 0.65L from the stern; as 2.5x/L at x metres from the stern to
        0.4L and as 1 ,0 — (x— 0.65L)/0.35L at x metres from the stern between
        0.651 and /,
          The IACS propose taking the wave induced shear force as:

            Hogging SF = O.SFjC/JStq, + 0.7) kN
            Sagging SF = -0.3F 2CLB(Q, + 0.7) kN


        F l and F 2 vary along the length of the ship. If F = 190 Q,/ [110(0,+
        0,7)], then moving from the stern forward in accordance with:

            Distance from stern  0   0.2-0.3    0.4-0.6    0.7-0.85    1
                 Length
                   F l          0     0.92^       0.7         1.0      0
                   F z          0     0.92        0.7         F        0
        Between the values quoted the variation is linear.
          The formulae apply to a wide range of ships but special steps are
        needed when a new vessel falls outside this range or has unusual design
        features that might affect longitudinal strength.
          The situation is kept under constant review and as more advanced
        computer analyses become available, as outlined later, they are adopted
        by the classification societies. Because they co-operate through IACS
        the classification societies' rules and their application are similar
        although they do vary in detail and should be consulted for the latest
        requirements when a design is being produced. The general result of
        the progress made in the study of ship strength has been more efficient
        and safer structures.


        SHEAR STRESSES

        So far attention has been focused on the longitudinal bending stress. It
        is also important to consider the shear stresses generated in the hull.
        The simple formula for shear stress in a beam at a point distant y from
        the neutral axis is:

            Shear stress = FAy/It

        where:
                     F = shear force
                     A - cross sectional area above y from the NA of
                          bending
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