Page 106 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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88                 SLENDER STRUCTURES AND AXIAL FLOW

                  integration over the domain [0,1] yields






                                                                                       (3.86)





                  in  which  the  orthonormality  of  the  eigenfunctions  was  utilized  (Le.  the  fact  that
                   JJ  @,@,   dt = S,,,  S,,  being  Kronecker’s delta),  as well  as the  fact that @r h:@,, A,
                                                                                   =
                  being  the  rth  dimensionless  eigenvalue  of  the  beam.  The  definite  integrals  may  be
                  evaluated in closed form, defining the following set of  constants:





                   Their values for some sets of  boundary conditions are given in Table 3.1, in  which the
                   a, are the constants associated with the 4,  [Bishop & Johnson 1960; cf. equation (2.28)].
                   The method for evaluating h,,,  c,,  and d,,  analytically is illustrated in Appendix B.
                     Equation (3.86) may be written in matrix form as follows:

                    q + [F + 2/3”2uB]Q + {A + yB + [u2 - r + n(l - 214  - y]C + yD}q = 0,  (3.88)

                   where  q = (41, q2, . . . , q~)~, F  and  A  are  diagonal  matrices with  elements  (ah: + a)
                   and  (A: + k),  respectively, and B, C and D are matrices with elements b,,,  c,,  and d,,,
                   respectively. This equation may be written in standard form,

                                             [Mlq + [CIQ + [Klq = 0                    (3.89)

                   cf. equation (2.1),  Section 2.1. Its  eigenvalues may  be  found in  various ways; e.g.  by
                   transforming  it  into  first-order form  by  the  procedure  leading from  equation (2.15) to
                   (2.17), and then to the standard eigenvalue problem of equation (2.18). The eigenvalues
                   may  be  obtained numerically, e.g.  by  the  IMSL  library subroutines or  those  given by
                   Press et aE.  (1992).


                   3.4  PIPES WITH SUPPORTED ENDS
                   3.4.1  Main theoretical results

                   We  first consider the simplest possible system: a simply-supported (or ‘pinned-pinned’)
                   horizontal pipe (y = 0) with zero dissipation, and with /? = 0.1, r = I7 = k  = 0 in equa-
                   tion (3.70). The dynamical behaviour of  this system with increasing dimensionless flow
                   velocity, u, is illustrated by the Argand diagram of Figure 3.9. It is recalled that %e(w) is
                   the dimensionless oscillation frequency, while 9am(w) is related to damping, the damping
                   ratio being ( = 9am(w)/%e(w). The general dynamical features already remarked upon in
                   Sections 3.2.1 and 3.2.3 are clearly seen: (i) since dissipation is absent in this example, the
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