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            Figure  is the time history of axial force of fender located at the center of the structure with gap 4.0cm,
            it can be  seen that  the  curve of axial  force is a discontinuous  line due to the existence  of mooring
            clearance between  the  fender and the  structure, the long period  wave curve with  short period  wave
            curve.
            Figure  and Fig.  is the time history of deflection of the free end and the center in the same case. It
            should be noted  that the two curves are similar but the phase is different, that is, the structure is not
            only moving as a rigid  body, but  also deflecting  as an elastic structure.  By  analyzing the frequency
            characteristic of the curve  data using  FFT program,  we  got the distribution  of frequency  spectrum
                                #                                                2
            shown in Fig., it should be noted that the frequency of the first peak and second peak are very close to
            the yawing period and the first elastic eigen frequency in the horizontal.






                                                                          (b) Damaged
                Figure 5:  Characteristic  of  fender
                        with clearance and model     Figure7:  Change  of  model  when  fender
                                                              was damaged
                                                                  TABLE 4
                                                   CALCULATION CASES FOR MOORING CLEARAP  r
                                                       I Clearanc  I Condition for load
                                                       le      I

               Figure 6:  Characteristic   of   fender
                        considering damage




                          om of fender al eo           -  -    Displacement of P210
                                                       :
                                                       :
                                                       -  0.15
                                                       ,"  0.1
                                                       0
                                          0             0.05
                                                          0
                                                        -0.05
                                                        -0. I
                                                        -0.15
             Figure 8:  Time history of axial force for a
                      selected fender
                                                    Figure 9:  Time  history  of  deflection  of
                                                            selected points on main structure
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