Page 311 - Marine Structural Design
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Chapter 14 Offshore Structures Under Impact Loads                     287

                  The characteristic length L, , is a function of the outer diameter, the length of the tube, and the
                  shape of indenture. In order to get an empirical equation, linear finite shell element analysis
                  results from Ueda et a1 (1989) and indentation tests conducted by Smith (1983) are analyzed.
                  A mean value is found to be:
                       L,   =  1.9D                                                   (14.3)
                  More  experimental or  numerical data  are  necessary to  get  a  more  rational  value  of  the
                  characteristic length L, .

                  When the load P is larger than the critical value Po. A permanent indentation will take place,
                  and the critical value can be determined using a rigid-plastic analysis for a pinch loaded ring
                  with length L, . The result obtained is:

                       P,  =  20,T2L,/D                                               (14.4)
                  where o, is the yield stress of the material.
                  The permanent indentation 6,  can be calculated using a semi-empirical equation. Through
                  energy  considerations and  curve  fitting  of  experimental  data,  Ellinas  and  Walker,  1983
                  obtained:
                       6,  =D( 37.5~~ )’                                              (14.5)
                                    T2


                  The  unloading  linear  deformation 6;  can  be  obtained by  multiplying the  linear  elastic
                  solution by a coefficient a:
                                   (:I
                       6;  =0.111&  - -                                               (14.6)
                                       :,

                  The  coefficient a will  be  less  than  or  equal  to  1.0 depending  on  the  deformation  at  the
                  unloading point.
                  Finally, the local displacement at the load point for a load larger than the Po  is calculated as:
                       s=s;  +6,                                                      (14.7)

                  14.2.3  Beam-Column Element for Modeling of the Struck Structure
                  A finite beam-column element as described in Chapter 12 of this Part is adopted to model the
                  affected structure.

                  14.2.4  Computational Procedure
                  The procedure described above has been implemented into the computer program SANDY
                  (Bai, 1991), three types of loads can be applied, to the simulated model, to obtain a collision
                  analysis of the affected structure.
                  Impact loads are applied at the node points and/or spatially distributed over the finite elements.
                  The time variation of these loads is given as input data before initiating a calculation. This
                  type of loading is used in Examples 14.1-14.3.
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