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Chapter 9 Buckling and Local Buckling of Tubular Members              185


                  As  described in  9.3.2.3,  there  exists no  one-to-one correspondence between plastic nodal
                  displacements  and  plastic  strains  at  a  nodal  point.  However,  plastic  strains  may  be
                  concentrated near  the  cross-section where  local  buckling  occurs.  So,  the  axial  strain  and
                  curvature at this cross-section are approximated by:
                       e=PfEA+e,,  +(up -uFr)flp                                      (9.87)
                       K=M/EI+KFr+(Op -OFr)/lP                                        (9.88)


                  lp in the above equations represents the length of plastic zone, and is taken to be equal to the
                  diameter D(=2R ) as in the case of a simplified method. Considering Eqs. (9.87) and (9.88),
                  the filly plastic interaction relationship reduces to:


                  The elasto-plastic stiffness matrix after local buckling occurs, is derived based on the filly
                  plastic interaction relationship expressed by Eq. (9.89).  The condition to maintain the plastic
                  state is written as:
                          ar     ar     ar     ar
                      dT=-dP+-dM+-du,        +-de,   = 0                              (9.90)
                           ap   a~     auP     a@,
                  or in the matrix form as:


                                                                                      (9.91)

                 where,  {dR) and  { dh,}  are the increment of nodal forces and plastic nodal displacements,
                 respectively, see Figure 9.12 and the following Equations:
                      (bj = {ar/ax,, ar/az,, aqa!}


                      4j = (ar/ax,, arjaz, , aqaM,}                                   (9.92)
                      vi = @q/hpi, ar/aYpi. arpPi}
                      vj = brp, j, aqh, I aqas, \                                     (9.93)


                 Here, considering ras a plastic potential, the increments of plastic nodal displacements are
                 given as

                                                                                      (9.94)


                 When only nodal point j is plastic, d;li = 0. Contrary to this, dAj = 0 when only node point i is
                 plastic.
                 On the other hand, the increments of nodal forces are expressed in terms of the elastic stiffness
                 matrix and the elastic components  of nodal displacement increments as follows:
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