Page 118 - Marine Structural Design
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94                                                Part I Structural Design Principles

                should be good enough. The total loading must be balanced so that the reaction forces at the
                boundaries approach zero.
                When  modeling,  the model  length of  the  ship  structure should be  sufficient to  minimize
                boundary condition effects over the analyzed area. ABS (2002) requires 3 cargo holds to be
                covered for models of  tankers,  bulk  carriers, or container ships;  LR  "Direct calculation -
                Guidance Notes" (1996) requires that 2 cargo holds be covered for the model of a bulk carrier.
                All continuous longitudinal elements should be restrained to remain plane under the effects of
                the hull girder bending and must be rotationally fixed about the vertical axis if the calculated
                deformations or forces are not available at the free ends of the model. Conditions of symmetry
                should be applied at each end of the finite element model. Rotation about the two axes in the
                plane of symmetry is to be constrained where there is symmetry imposed at the centerline or at
                the ends of the model. The model should be supported vertically by distributed springs with
                shipsides and longitudinal bulkheads at the intersections of the transverse bulkheads.
                5.3.3   Type of Elements

                The types of elements are chosen to provide a satisfactory representation of the deflections and
                stress distributions within the structure. The conventional frame analysis may be carried out
                with  a  beam  model.  It  has  significant  advantages  for  its  modeling  simplicity  and
                computational  efficiency.  However,  thanks  to  the  availability  of  powerhl  computers,
                computational efficiency is no longer a concern. More refined and accurate element types can
                be used.
                In  a  research conducted by the ISSC, Zillottto et al. (1991),  nine different finite element
                models were applied to different combinations of beams, trusses, rods, membranes, planes,
                and shell elements. A considerable scatter was observed in the results. The conclusion was that
                a detailed analysis of the deformations and stress levels in all the elements of the transverse
                frames should be performed using a refined finite element model for all the different types of
                structures and ships.
                In  "Direct  Calculation-Guidance Notes",  LR  (1996)  suggests that  all  areas of the  plating
                should be modeled by shell elements, secondary stiffeners by line elements (bars  or rods),
                double bottom girders and floors by  three or more plate elements over the depth of these
                members, and side shells by plate or bar elements.
                In general, if the structure is not subjected to lateral bending, membrane and rod elements may
                be  applied. Otherwise, plate and beam elements, which have both bending and membrane
                resistance, should be employed. The selection of element types depends on many aspects, such
                as the type of structure, the load application approach, the type of analysis performed, the
                results generated, and the accuracy expected. There is no substitute for engineering judgement.
                5.3.4   Post-Processing
                The design is a complicated and iterative process in which building and solving a FE model is
                simply the  first  step.  A  more  important step  is  that  designers use  their  knowledge  and
                judgment to analyze the results and, if necessary, redesign or reinforce the structure.
                First, the engineer must ensure that the results calculated by the FE program are reasonable,
                and that the model and the load application are correct. This can be achieved by plotting stress
                contour, the deformation, the reactions & applied load equilibrium, force & moment diagrams,
                etc. The next step is to check the strength of the structure against relevant design criteria. Load
                combinations and stress combinations are not always straightforward. Assumptions are usually
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