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134               SLENDER STRUCTURES AND AXIAL FLOW

                      All  measurements were  straightforward, except  perhaps  the  measurement of  EZ for
                    rubber pipes, required in  the  determination of  the  dimensionless flow  velocity,  u. The
                    techniques utilized for this are summarized in Appendix D.
                      Some of the general observations on the dynamical behaviour of this system are worth
                    giving in some detail; they are similar to those made by  other researchers in  the experi-
                    ments to be discussed later.
                      Small flow velocities increased the  damping of  the  system, and  oscillations induced
                    by  light  taps  close  to  the  free  end,  which  were  still  of  the  general  shape  of  the  first
                    cantilever  mode,  decayed  much  faster.  At  somewhat larger flow velocities the  system
                    became overdamped and any displacement of  the pipe was followed by  a return to rest
                    without  any  oscillatory motion. In  some cases physical contact  of  the  free end  of  the
                    pipe with the hand, momentarily transforming the system to one supported at both ends,
                    caused  the  pipe  to  buckle  by  bowing  out  near  the  middle. When  contact  was  broken
                    suddenly, the pipe returned rapidly to its position of rest, but when the hand was removed
                    only  slowly,  the  pipe  pressed  against  and  followed  the  hand  with  the  result  that  the
                    timid observer was soon faced with a stream of fluid directed against himself (or nearby
                    colleagues!) - this,  as already remarked, being a demonstration of  a negative-stiffness
                    (divergence) instability.
                      At  still higher  flow velocities, light taps resulted in  heavily damped  oscillation with
                    a form rather  more  like that  of  the  second cantilever mode  than  the  first. As  the  flow
                    velocity  increased  further,  the  system  became  less  heavily  damped  until  at  a  certain
                    critical velocity of  flow the disturbance produced by  lightly tapping the pipe grew into a
                    self-supporting oscillation. If no outside disturbance was introduced, the system eventually
                    became unstable spontaneously. This usually occurred at measurably higher flow velocities
                    than  were  sufficient for  ‘induced’ instability  to  take  place,  particularly  in  the  case  of
                    rubber pipes. Further increase of  the flow velocity beyond the stability limit resulted in
                    an increase in both the amplitude and frequency of  oscillation.
                      When decreasing the  flow velocity, it  was noted that  oscillation persisted below  the
                    point where instability, spontaneous or  ‘induced’, first occurred. This, and also the fact
                    that  in  some  cases  the  onset  of  instability depended  on  the  amplitude  of  the  applied
                    disturbance, indicated that the experimental systems behaved in general nonlinearly.
                      The mode of  deformation of  the unstable system was recorded with a cinC-camera in
                    a few selected typical cases and a number of  successive frames of the film are shown in
                    Figures 3.45(a-c).  In general, for very small values of ,%  the modal form was essentially
                    that of the first cantilever mode, with a small component of the second. For higher values
                    of p, the second cantilever mode became more prominent, and for fi > 0.3 approximately
                    the  third  mode  became apparent  [e.g. see frame  8 of  Figurc 3.45(c)]. In  all  cases, the
                    tangent to the free end of the pipe sloped backwards to the direction of motion of the free
                    end over the greater part of  a cycle of  oscillation. This  ‘dragging’ motion was predicted
                    to be necessary for flutter, in conjunction with the energy considerations of Section 3.2.2.
                      Indeed,  all  observations  described are  in  agreement with  the  theoretical predictions
                    of  Sections 3.5.1 and 3.5.2. However, two additional comments should be  made. First,
                    the  dynamical  behaviour  of  the  system  is,  to  some  extent,  nonlinear - as  noted
                    above - suggesting that the Hopf bifurcation is subcritical. Second, according to linear
                    theory,  once  instability  is  developed,  the  amplitude  should  increase  without  limit;  of
                    course, once the amplitude becomes large, nonlinear forces come into play, and in  this
                    case evidently their net effect is to limit the amplitude, thereby establishing a limit cycle.
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