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Chapter 9 Buckling and Local Buckling of Tubular Members               175


                        = 0-7 iW)                                                     (9.38)
                                     G=1.21&

                  The axial strain in a tube wall fiber where local buckling has occurred may be expressed as:

                       E = E,  + (1/2S)f(dWb/drfdr  =  + (7?/416/3)2                  (9.39)
                  On the other hand, considering the equilibrium condition of a bending moment in a strip with
                  its unit width cut out fiom the tube wall, the following equation is obtained. (See Figure 9.16
                  (b)):
                       AF,6-2dM,  =o                                                  (9.40)
                  The interaction between the strips is not considered when Eq. (9.40) is derived. According to
                  the  assumptions previously  mentioned,  local  buckling  takes  place  in  the  plastic  region.
                  Consequently, AF, and AM, should satisfy the hlly plastic interaction relationships, which
                  are expressed as:
                       A M,/M~ = 1 -(A F,/F,)~                                        (9.41)
                  where,

                       Fo =tu,
                       M, = t2cy /4                                                   (9.42)
                  Using  Eqs.  (9.39),  (9.40), and  (9.41), the  stress-strain and  local  lateral  deflection  stress
                  relationships may be obtained as follows:
                       c/o1. = pi2 - $2                                               (9.43)

                       &/t = (1 - +Y  Y /(2+,  )                                      (9.44)
                  where,

                       p = (4s/rdh/G                                                  (9.45)
                  The stress-strain relationship represented by Eq.  (9.43) is schematically illustrated in Figure
                  9.16  (c).  Applying  this  model,  the  stress  distributions  for  tube  cross-section  after  the
                  occurrence  of local buckling are represented as in Figure 9.17. For a case A' stress distribution,
                  the following relationships are derived in place of Eqs. (9.22) and (9.23).
                      &I+ A)= f2 + f; +(c +c;h                                        (9.46)
                      P(@+eo)=f, +f:+V4 +f,v)/Cr,  +v)+fs                             (9.47)

                  where,
                      f; = 2ayR2t(g, -a)cosa,                                         (9.48)
                      f: = 20,  Rt(g, - R sin a)
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