Page 91 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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74                SLENDER STRUCTURES AND AXIAL FLOW

                    [Parenthetically, a  more  'fluid  mechanical'  derivation  given  by  Pa'idoussis  & Issid
                  (1974) will be outlined here, in which an element of the pipe 6s is considered containing
                  fluid of volume W. The rate of  change of momentum over W may be written as

                                                                                       (3.30)

                  where d@V  is a small element within 6"lr. Then, by  making the plug flow approximation,
                  the velocity V,  may be approximated by  (3.27). Therefore,


                                at    dt

                                                                                   k.  (3.31)

                  Hence, equation (3.30) yields

                                     dM      dU
                                     -=M-&i+M                                          (3.32)
                                      dt      dt
                  which corresponds to the acceleration as given by (3.28).]
                    A derivation  in  which  the radial  dimensions of  the pipe are not  ignored is  given in
                  Section 4.2, but leads to the same form as above. Therefore, recalling that s 2: x, by using
                  (3.28) or (3.32) one obtains the first two of the following equations:





                  the last equation above is the lateral acceleration of  the pipe and requires no explanation.
                  Hence, combining (3.19), (3.21), (3.22) and (3.33) one obtains
                                                 a
                                        I---
                              E  -+E
                             ( *it  )  a#       ax
                                                      aw     a2w
                                                   +c-++-=o.                           (3.34)
                                                       at     at*
                    Also, adding equations (3.18) and (3.20) and using (3.33) yields


                                                                                       (3.35)
                  which integrated from x  to L becomes
                                                                      1
                          (T - pA)l   - (T - PA) =          - (M +m)g  (L -x).         (3.36)
                                  x=L
                  If the flexible pipe discharges the fluid to atmosphere at x = L - the situation shown in
                  Figure 3.l(b,c) - T, which is then entirely due to fluid friction, is zero at x  = L; unless
                  there is an externally applied tension, denoted by T - as could be the case for the system
                  of Figure 3.l(a).  The pressure,  p. at x  = L  will  also be  zero, unless the pipe  does not
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