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114               SLENDER STRUCTURES AND AXIAL FLOW

                   the first-mode shape contains appreciable second-mode content, the second-mode shape
                   third-mode content, and so on. Nevertheless, the present appellation is clearly a reasonable
                   one. Another important point is that, similarly to the pipe with supported ends, these are
                   not stationary, classical modes with fixed nodal points, but contain appreciable travelling
                   wave components, to be discussed with the experiments in Section 3.5.6.
                     The  critical  flow  velocity,  ucf  as  a  function  of  #?  is  shown  in  Figure 3.30;+ there
                   exists  a  similar curve  for  the  corresponding frequency  at  u = u,f, labelled wcf  - see
                   Figure 3.35. It is  clear that,  ucf depends  strongly on 6. Furthermore, the  ucf and wcf
                   curves contain a set of S-shaped segments. By referring to Figure 3.28 it is recognized that
                   they are associated with the instability  -restabilization-instability  sequence discussed in
                   the foregoing; hence, in Figure 3.30, the negative-slope portions of the curve correspond
                   to thresholds of restabilization. If an experiment could be conceived in which the material
                   damping is zero and #?  could be varied in very small steps, then around these points there
                   would be  ‘jumps’ in u,f; e.g. for #?  in the vicinity of 0.69, from u,.. 2:  11 to ucf 2: 12.8
                   for a very small increase in #?. The values of #?  associated with these S-shaped segments
                   of  the stability curve (at #?  2: 0.30, 0.69, 0.92) will be found to be associated with a large
                   number of perplexing linear and nonlinear characteristics of the system - in the sense of
                   acting as separatrices for differing dynamical behaviour. Yet, the origin of  their existence
                   is not fully understood (see Section 3.5.4). As  #I -+  1, more and more S-shaped jumps
                   are encountered. Mukhin has shown that for #?  = 1  no flutter solution may be possible,
                   i.e. ucf 4 00  (Mukhin 1965; Lottati & Kornecki 1986).





























                   Figure 3.30  The  dimensionless  critical  flow  velocity  for  flutter,  urj, of  a  cantilevered  pipe
                      conveying fluid, as a function of B, for y = 01  = (T = k = 0 (Gregory & Paldoussis 1966a).
                     Nevertheless, it appears that  these jumps  are related  in  some way  to mode  content.
                   This is made clear by Figure 3.31 in which, in addition to results obtained by the method

                     +Numerically, such curves are computed by determining fi for each assumed ucj, rather than vice versa
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