Page 166 - Marine Structural Design
P. 166

142                                                     Part XI Ultimate Strength

                 Then  the  deflection w, due to  the  initial  deformation is  determined from  the  differential
                 equation:

                      EI-    -                                                        (8.4)

                 Substituting Eq. (8.1) into Eq. (8.4), we may obtain:
                      d2wl
                                            m
                      -+    k2w, = -k2w,,,  sin-
                       dX2                  I
                 where,



                 The general solution of Eq. (8.5) is:
                                            1         .m
                      wI = Asinkx+Bcoskx+-      w,,,  sin -
                                          ?r2
                                          --   1        I
                                          k212
                 To satisfy the boundary condition (w, = 0  for  x = 0  and   x = 1)for any value of k, A =
                 B = 0.  Also, by using the notationa for the ratio of the longitudinal force to its critical value:




                 where,
                          Z’EI
                      PE =-
                           I2
                 we obtain the following:
                           a         m
                      w, =-   wonax sin -
                          1-a         I
                 The final form of the deflection curve is:

                                        m
                                             a
                                                      .m
                      w=wo+wl =w,,,sin-++w,,,sin-=~sin-            m
                                         I   1-a        I   1-a    I                  (8.9)
                 This equation shows that the initial deflection w,,,  at the middle of the column is magnified
                            a
                 at the ratio - the action of the longitudinal compressive force. When the compressive
                               by
                          1-a
                 force P approaches its critical value, a approaches 8.0, the deflection w increases infinitely.
                 Substituting Eq. (8.9) into Eq. (8.3), we obtain:
                                                                                     (8.10)
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