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PIPES CONVEYING FLUID: LINEAR DYNAMICS I1              23 1

             (b) Cantilevered pipes and outflow models

             Unlike  pipes  with  fixed  ends,  a  cantilevered  pipe  discharges  the  fluid  freely  from
             its  downstream  end.  The  emerging jet  continues  its  sinuous  path  in  the  ambient  air,
             [Figure 4.16(b)], as briefly  discussed in  Section 3.5.8. The  motion  of  the  cantilever is
             therefore coupled with that of the downstream jet (at least in this kind of formulation) - as
             first discussed by Shayo & Ellen (1978). Thus, in a study of the flow-induced instability
             of  a  cantilevered pipe,  it  becomes necessary to  construct an  artificial  ‘outflow model’
             which  describes the manner in  which W(6) and hence the perturbations in  the  fluid are
             attenuated beyond the free end of  the pipe.
               For long pipes conveying fluid, the plug-flow model is fully expected to give reasonable
             approximations to  the  fluid-dynamic forces,  and  hence  to  predict  reasonably  well  the
             dynamical  behaviour  of  the  system.  Moreover,  the  results  have  been  found  to  be  in
             good  agreement with  experiments, and  the  plug-flow  model  may  be  considered to  be
             quite adequate for  long cantilevers conveying fluid. Therefore, the  following approach
             is  adopted: different outflow-model functions Gn(6) and various values of  Z(1  > 1) are
             tried and adjusted, so that the generalized fluid-dynamic forces (4.67) obtained by refined
             fluid mechanics agree with those obtained by  simple fluid mechanics [plug-flow model
             with  equations (4.49)]  for  a  long  cantihered pipe. It  is  then  assumed  that  the  same
             outflow-model functions G,(e) and  value of  1  would apply for short pipes - indeed to
             the very short cantilevered pipes which are the subject of this section. The validity of this
             assumption is tested, partially at least, by  comparison with  experimental measurements
             (Section 4.4.8).  Following  the  mathematical formulation  suggested by  Shayo  & Ellen
             (1978) for both the beam-  and  shell-mode dynamical behaviour of  a cantilevered shell
             conveying fluid, three different downstream flow  models are tried for  the  cantilevered
             tubular beam;  their  characteristics are  summarized in  Table 4.2,  together  with  the  ‘no
             model’ situation, in  which the deflection of  the perturbation in the fluid is  supposed to
             vanish  abruptly at 6 = I  = 1; for the  ‘first’, ‘second’ and  ‘third’ models, the motion  of
             the  fluid  beyond  the  free  end  is  described  by  progressively higher-order polynomials
             of  the  fluid-jet deflection. The  ‘first model’ is  Shayo & Ellen’s  ‘collector pipe model’
             (Section 3.5.8). The  ‘second model’ is described mathematically by
                                  -1                       -1
                 Gn(<) = Y,(1)  [I  -     + YA(1) [(c - 1) -           forl<C(/,
                                  (I  - 1)*                (1 - 1)
                                                                                  (4.68)



             The ‘third model’, which involves a cubic polynomial in 6, is given in detail in Luu (1983);
             this model transcends physical reality by unjustifiably specifying a zero slope for the free
             jet far downstream (Table 4.2). Calculations done for a very long cantilever (A = lo’*)
             according to the various models of Table 4.2* show that the second model, equation (4.68),
             with 1 = 2.8 gives optimum results, as may be seen in Table 4.3. The second and third modes
             were also tested, and the second model with I = 2.8 again gives the best results. Hence, it

               +In these calculations, the  ?((I  used  in (4.67) are the eigenfunctions of  clamped-free  Timoshenko beam
             without  flow; the integration range for ?i is [-150,  1501 and the integration step fi = 2. These give convergent
             results and have been used  thruughout in calculations for cantilevered pipes.
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