Page 102 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
P. 102

PIPES CONVEYING FLUID: LINEAR DYNAMICS I                85

              (a) First method

             The  simplest  form  of  the  equation  of  motion,  equation (3.1), will  be  considered  first,
             which in dimensionless form becomes
                                     +
                                  a417    a2q         a2r   a2r
                                             +
                                 - u  - 2pu               +--0,                   (3.76)
                                  at4     ap         ~  acat   at2
             subject  to  the  appropriate  boundary  conditions;  e.g.  for  a  pipe  with  simply-supported
             ('pinned')  ends,
                                                                                  (3.77)

             while for a cantilevered pipe,




                                                                                  (3.78)


               Consider now solutions of the form

                                        r~, ~WO)~'"'I,                            (3.79)
                                            r)
                                              =
             where  w  is  the  dimensionless  circular  frequency  defined by  (3.73).  In  general,  w  will
             be  complex,  and  the  system  will  be  stable  or  unstable  accordingly  as  the  imaginary
             component  of  w, 9m(w), is  positive  or  negative;  in  the  case  of  neutral  stability  w  is
             wholly real. Substituting (3.79) into (3.76) leads to

                                                                                  (3.80)

               Next, we take a trial solution
                                             Y(6) = A&,                           (3.81)
             where A  is a constant. When this is substituted into equation (3.80), the equation deter-
             mining the permissible values of the exponent a is obtained, namely

                                    a4  - u2,2   - 2pum - 02 = 0,                 (3.82)
             and  since this  equation  is  of  fourth  degree,  the  complete  solution of  (3.76) is  given  in
             general by


                                                                                  (3.83)

             in which the four A,  must be determined from the boundary conditions. This is illustrated
             here for the cantilevered system. Making use of  (3.78), we find
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