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PIPES CONVEYING FLUID: LINEAR DYNAMICS I                61

























                                                                                      1.







                Figure 3.1  (a) A  pipe  with  supported  (clamped)  ends  conveying  fluid,  where  longitudinal
                movement at the supports is prevented; (b) the same system, but with axial sliding permitted; (c) a
                cantilevered, continuously flexible pipe conveying  fluid;  (d) a two-degree-of-freedom articulated
                version  of  the  cantilevered system, in  which RL is the position  vector of  the  free end, measured
                      from its position of  equilibrium, and  IL  is the unit vector tangent to the free end.

                it is clear how the terms related to fluid acceleration,

                           (;+U~}[$+Ug]  = [U  ,,+ZU-+-                              (3.2)
                                                         a2w
                                                                  axat a2w   at2  ’

                arise in equation (3.1). Here, however, the equation of motion will be considered in purely
                physical terms.
                  The  first  term  in  equation (3.1)  is  the  flexural  restoring  force.  Upon  recalling  that
                a2w/ax2 - l/%, where 3 is the local radius of curvature, it is obvious that the second term
                is associated with centrifugal forces as the fluid flows in curved portions of the pipe - see
                Figure 3.l(a-c). Similarly, re-writing a2w/axat = %/at  = a, the local angular velocity, it
                is clear that the third term is associated with Coriolis effects: the fluid flows longitudinally
                with velocity  Ui, while sections of the pipe rotate with  -Qj, where j is normal to (into)
                the plane of the paper; hence -2Qj  x  Ui terms arise. The last term represents the inertial
                force of the fluid-filled pipe.
                  Equation  (3.1) may  be compared to the equation of  motion of  a beam  subjected to  a
                compressive load, P,
                                                  a2w
                                          a4pv           a2w
                                        EI-  + P-    +m--  = 0,                      (3.3)
                                           a.r4   ax2     at2
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