Page 323 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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304               SLENDER STRUCTURES AND AXIAL FLOW

                   0, is
                               afi”” + q””  +   u  - f - y(1 - 6) - id   (v’)~ dt}  q”

                                           {2
                                                                                        (5.80)

                   with
                                                   d = AL2/I,                           (5.81)

                   all other quantities being  as in  (3.71),  (5.38) and (5.44). Most of  the  detailed work is
                   done with a simplified form of  (5.80) by taking r = y  = 0 and neglecting the nonlinear
                   dissipative term, namely

                              + $”’ + { *2  -  I’ (q’)’  d:}   q” + 2p1I2ulj’ + (TG + ij  = 0,   (5.82)

                   for a simply-supported (pinned-pinned)  pipe - thus satisfying q = q”  = 0 at 6 = 0, 1.
                     Holmes considers the dynamics of the system in two ways, via (a)$nite  dimensional
                   analysis and (b) in$nite  dimensional analysis, to be outlined in what follows. Then, some
                   interesting work by Lunn (1982) is discussed in (c), leading to (d) the final conclusion.
                   (a) Finite dimensional analysis

                   For  equation (5.82),  a  two-mode  Galerkin  discretization of  the  simply-supported pipe
                   system is obtained via ~(6, t) = E[& sin(rn()]q,(t),  r = I, 2. Converting this to first-
                   order form, leads to the following simple four-dimensional system:

                          41  = Ply   42 = P2>
                                 2
                                    2
                                        2
                            = -X  (n - U )SI - (an4 + a)pl + ~p   up2 - ;dn2(q: + 4q;)q1,  (5.83)
                                                            16  112
                   It is seen that the nonlinearities are of  the stiffening cubic type (of the same sign as the
                   linear stiffness), which helps explain the global stability of  the system.
                     It is useful here to refresh the reader’s mind as to the linear dynamics of the system.
                   Since damping is present  (a, o # 0), the  eigenvalues for  u = 0 are complex conjugate
                   pairs with negative real parts (Figure 2.10). Here the notation introduced by Holmes is
                   utilized,  in  which  such  eigenvalues  are  denoted  by  the  quartet  h = I-.  -, -, -},  the
                   signs being those of the real parts of the eigenvalues; a + means that one of the eigen-
                   values  has  positive real  part,  while  0 denotes  a  zero real  part.  As  u  is  increased, the
                   first  bifurcation  occurs  at  u = n (Section 3.4.1);  it  is  a  pitchfork  bifurcation,  leading
                   to divergence, as shown in Figure 5.4  (cf. Figures 3.9  and  3.14). Hence, for  u > n we
                   have h = [+, -, -,  -).  The solution of equations (5.83) shows that two new fixed points
                   are generated for  u > n, located increasingly farther away from the origin. The numer-
                   ical solutions for a = (T = 0.01,   = 0.2, are shown in  Figure 5.5, together with centre
                   manifold predictions, which will be discussed next.
                     At the critical point where the bifurcation occurs, the four-dimensional system (5.83)
                   is projected onto the  centre manifold (Appendices F.2 and  H.l), which in  this  case  is
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