Page 184 - Marine Structural Design
P. 184

160                                                      Part II Ultimate Strength



                                         P
                                          -

                                       40


                                                            - tension
                                       20                      8
                                                            --- I  conpression

                                                                     *
                                        0       0.2      0.4     0.6
                                                                 E (%)


                             Figure 9.3   (a) Stress-strain Curves for Small Scale Test Specimens, A
                                        Series
                 The compressive material tests were conducted using the  stub pipe. The length of the test
                 specimen was  selected  such that  column  buckling would  not  be  a  concern. The  selected
                 specimen length is 300 mm  for all of the test specimens. 4 pieces of bi-axial strain gauges
                 were put on the central cross-sections of the test specimens. The nominal stress-strain relations
                 are plotted in Figure 9.3 in dotted lines. Because shell mode buckling occurred in the upper or
                 lower edges occurred, strain-strain relation was measured up to the strain level of  1 %. The
                 obtained yield strength was given in Table 9.3.
                 Due to the tensile expansion applied in manufacturing the specimens along the longitudinal
                 direction, significant Bauschinger's effect was observed. There is little strain hardening effect
                 in the tensile side of the stress-strain relations. On the other hand, significant strain-hardening
                 effect was observed for the compressive side. As shown in the stress-strain curves, there is a
                 significant difference between the material properties in tensile side and in compressive side.
                 This difference in material properties could be one of the main reasons for the difference
                 between the test results and  analytical solutions for the load-deflection curves and  load-end
                 shortening curves.  Heat  treatment should probably have been  introduced to  eliminate the
                 differences in the material properties for tensile and  compressive sides,  and to  reduce the
                 Bauschinger's effect. However, due to the potential of buckling of the thin-walled pipe, such a
                 heat treatment was not applied.
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