Page 284 - Marine Structural Design
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260                                                     Part II Ultimate Strength


                 Each plastified node is checked for unloading. For nodes in non-linear spring elements as well
                 as for shear panel elements, unloading is detected when the load increment and the load have
                 different  signs.  For  all  elements with  unloading  nodes,  the  stifmess is  changed  and  the
                 procedure is continued from point (0.

                 When no further unloading is detected, the increments of displacement are obtained. Then the
                 internal forces for each element are calculated. For each elastic element, a check may be made
                 to determine whether yielding occurs during the step. If this is the case, the increment for that
                 element is divided into a part that is treated elastically and a part that is treated like plastic.
                 The increment in the internal force for the element is calculated from:
                      (uk} = factor  [KE ldu) + (1 - fuctorpc, Xdu)                 (13.26)
                 wherefactor is the elastic fraction of the increment.
                 Unloading is again checked.
                 If either loading or unloading takes place, and no kind of iteration is carried out, the change of
                 state gives rise to unbalanced forces, which should be added to the load in the next step. This
                 unbalanced force is calculated to be the difference in internal forces due to changes in the
                 elastic-plastic state.  This gives place to  yielding (dx) = (1 - fuctorNKE]- [Kp Ndu} and  to
                 unloading {q) = ([K, ] - [KE Ndu}.
                 Note that the global set of equations remains unchanged due to plastification in elements, this
                 means that the influence on the global situation from one node changing state, is disregarded.
                 A revision is made to determine whether any elements have tom.  If this is the case, these
                 elements are removed and their internal forces are added as unbalanced loads in the next step.
                 When the step is accepted, a new increment begins at point (a).

                 13.3  Analytical Equations for Hull Girder Ultimate Strength

                 Buckling and  collapse strength of hull girders under bending may be predicted as the fully
                 plastic moment, the  initial  yield  moment,  and the  progressive collapse moment.  The  last
                 includes buckling and post-buckling strength of individual components of the hull girder. The
                 fully plastic mode provides an upper bound of the ultimate strength, which is never attained in
                 a hull of normal configurations. The initial yield mode assumes that buckling does not occur
                 prior to yielding. The initial yield strength is a function of the elastic section modulus of the
                 hull girder and yield strength of the material.
                 In this section, an ultimate strength equation is proposed to account for the effects of lateral
                 pressures, bi-axial loading, and shear stress using analytical solutions.  The ultimate strength
                 equation  is  then  compared  to  the  sophisticated approach  described in  Section  13.4.  The
                 ultimate strength equation may be applied for the quantification of structural risks of aging
                 ships with corrosion and fatigue defects, see Parts IV and I of this book.
                 13.3.1  Ultimate Moment Capacity Based on Elastic Section Modulus

                 In the initial yield moment approach, it is assumed that the ultimate strength of the hull girder
                 is reached when the deck (alone) has yielded. Premature buckling is assumed not to occur. In
                 this approach, the elastic section modulus is the primary factor for measuring the longitudinal
                 bending strength of the hull. With these assumptions, the initial yield moment can be written
                 as:
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