Page 196 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
P. 196

178               SLENDER STRUCTURES AND AXIAL, FLOW






























                                 -1.0

                    Figure 3.72  The time evolution of disturbance at 6 = 0 for an infinitely long pipe on an elastic
                    foundation with (a) k = 0 and (b) k  = 6.30, for u = 0.160, CT = l7 = 0 (Stein & Tobriner 1970).
                    is much smaller. However, for smaller k  (not shown here), neither a well-defined wave
                    packet nor an axis of symmetry develops.
                      Finally, it is stressed that the calculations in Figures 3.72-3.74  have all been done with
                    cr = 0. This should be borne in mind when considering wave propagation in real systems,
                    in which dissipation is always present.


                    3.7.3  Periodically supported pipes
                    An  excellent treatment of  the subject was provided by  Chen (1972a), an outline of  the
                    salient features of which is given in what follows.
                      Suppose  that  the  pipe  is  simply-supported periodically  at N  supports, as  shown in
                    Figure 3.75(a), where N  may be finite or tend to infinity. The equation of motion is
                                                       +
                                    Q”’’ + (u2 - r + WQ” 2p’/2ui7’ + ij  = q+(6)eiur,   (3.149)
                    a version of (3.70); the term on the right side represents a possible forcing function.
                      Considering two neighbouring spans of the pipe on either side of the jth support, and
                    denoting quantities on its left without a bar and those on its right with a bar, the boundary
                    conditions to be satisfied are

                                 ~(0) ~(1) = 0,     ~”(0) -aj-1,      ~”(1) = -aj,
                                     =
                                                         =
                                                                                       (3.150a)
                                 -                  -1’
                                 Q(O> = ~(1) = 0,   Q (0) = -Zj,    $’(I)  = -Zj+1,
                                                    Q’U) = 77’(0),                     (3.150b)
   191   192   193   194   195   196   197   198   199   200   201