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PIPES CONVEYING FLUID: LINEAR  DYNAMICS I               91


                             I    1     I   1-1    I   p-         I   '-/         r
                                                             I
                                                        I
                 16  -                                                                -
                   -                               .q0                                -
                      '-; 8.5                     d5 Combined 1st and 2nd modes
                  8-    ,                                                             -
                   - 6.5, I' '                                                 3rd mode
                        e 8.96                                                        -
                             9
               3             --          9.1                 -  2nd mode        2J0
              z 0'              -                                  -pzy/           A
               ..
                     2.rr"'  :.28   6  .  6  2  7  T--                                -
                                                              0
                                  I st mode
                                                 19.5                                 -
                      8
                 -8   6.5f:                       \                                   -
                                                   \ 10
                -16  -                                                                -
                                                  ,\&             ,,
                             I    I                                   -/         '    J
                        0         4          16        20
              Figure 3.11  Dimensionless  complex  frequency diagram  for  a clamped-clamped  pipe;   = 0.5
              and r = l7  = a!  = (r = k  = y  = 0. The loci that actually lie on the axes have been drawn slightly
                    off  the axes but parallel to them for the sake of clarity (Pai'doussis  & Issid  1974).

              of  Section 3.3.6(a)  and  obtain  the  full  curve  of  the  first-mode o versus  u, up  to  uCd,
              by  computer.  However,  more  interesting  methods  have  also  been  employed:  the  direct
              method of  Lyapunov (Appendix F.1.3) by  Movchan (1965), and the methods of  integral
              equations by Jones & Goodwin (1 97 1). Also, utilizing a perturbation method, Handleman
              (1955) determines  the  dependence  of  w  on  u  in  the  vicinity  of  u = 0 and  u = ucd. In
              all cases the simplest form of the equation of motions is considered, equation (3.1), and
              in all cases but the last for pinned-pinned  pipes only. Finally, Niordson (1953) presents
              an  elegant  wave  solution to  the  more  general  problem  of  a thin-walled  pipe,  modelled
              as  a shell  (Chapter 7); the required  results  for beam-like  motions  are then  obtained  by
              considering the n = 1 mode of  the shell - see Figure 2.7(c).
                The post-divergence dynamical behaviour of these systems, i.e. for u > U,d,  is of consid-
              erable interest. It should, however, immediately be remarked that strictly, linear theory is
              applicable  only up  to  the first loss of  stability. The reason  for this is that, in the linear
              equation  of  motion,  it is required  that  motions  be  small,  in  the  vicinity of  the  equilib-
              rium  state, while  for  u > u,d  the  system has diverged  away from  that  state.'  However,
              in  some cases (e.g. in Chapter S), the buckled state is not so far away from the original
              stable equilibrium configuration, and then linear theory is capable of predicting the post-
              divergence dynamics of the system reasonably well. Hence, it is not pointless to examine
              the post-divergence dynamics as predicted by  linear theory.
                It  is  seen  in  Figures 3.9  and  3.10  (,!?  = 0.1)  that  the  simply-supported  and  clamped
              systems develop divergence in the second mode at u = 2n and 8.99, respectively. Then,
              the loci of the two modes coalesce on the Sm(w)-axis and, at slightly higher u (u 2 6.38

                'Of  course, the  stability  of the original equilibrium as predicted  by  linear theory  is always valid, but other
              states emerge once nonlinear effects are considered.
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