Page 395 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
P. 395

PIPES CONVEYING FLUID: NONLINEAR AND CHAOTIC DYNAMICS          371


               pipe  in  the  course  of  oscillation  and  (ii) to  ensure  that  it  is  not  overtightened  onto  thc
               pipe, thus deforming its free end.
                 Several  elastomer  pipes  were  used  (typically,  Di = 6.3 mm,  Do = 15.7mm,  L =
               470mm),  giving  fi = 0.125-0.150  and  y  2: 20,  and  eight  different  end-masses,  made
               of  plastic  or  metal,  JM. = 2.4-37.8  g;  this  corresponds  to  values  of  the  dimensionless
               added mass,

                                                                                   (5.139)


               ranging from p = 0.023 to 0.380.
                 Typical results  related  to  the flutter threshold,  which exhibits  the characteristics  of  a
               Hopf bifurcation,  are given in Figure 5.44(a).  It  is remarked that (i) the additional mass
               destabilizes the system, in agreement with Hill & Swanson's  findings (Figure 3.68), and
               (ii) there is considerable hysteresis in the critical u obtained with increasing and decreasing
               flow, suggesting that the Hopf bifurcation is subcritical.


                  0.4
                                                            4  ,    I                  t


                  0.3
                                                            3-










                  0.0                                                                  I
                                                              1.5   2   2.5   3   3.5   4
                     (a)         Flow velocity, if,,         (b)    Flow velocity, (u&~
               Figure 5.44  (a) Experimental critical flow velocity for the onset of flutter as a function of  p [equa-
               tion  (5.1391 for  the  system  of  Figure 5.43(a): ---, linear theory; +, experiment for increasing
               u,  the  error  bar  indicating  maximum  repeatability  variations;  0, experiment  for  decreasing  u,
               (mean  value)  (PaYdoussis & Semler  1998).  (b)  Similar  observations  over  a  larger  range  of  p,
                               with  (u~)~~ V,,/(gL)'/*, by  Copeland & Moon (1992).
                                       =

                 Similar results from Copeland & Moon (1992) are shown in Figure 5-44(b) for a much
               wider  range  of  p. Motions  in  this  case  too  were  mostly  planar  at  the  onset  of  flutter
               [see Section 5.8.3(b)].  It  is  seen that,  contrary  to  the effect  of  smaller  p, the  presence
               of  end-masses with  p > 0.5 approximately stabilizes  the system vis-&vis  /* = 0. These
               results also display hysteresis and suggest a subcritical Hopf bifurcation. The pipes in this
               case were very long and slender (L - 1 m, LIDi 2:  125); according to theory (for p = 0)
               such  slender pipes  should lose  stability by  a supercritical Hopf  bifurcation  [Figure 5.20
               and Bajaj et al. (1980)l.
   390   391   392   393   394   395   396   397   398   399   400