Page 529 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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SOME OF THE BASIC METHODS OF NONLINEAR DYNAMICS             499

               where yc E ker L and ys E range L*, and to define two orthogonal operators, P onto the
               range of L, and the complementary operator I - P, where I is the identity operator, such
               that (Golubitsky & Schaeffer 1985)
                                                                                  (F. 84a)

                                                                                  (F.84b)
               in which y is replaced by (F.83). We can then apply the implicit function theorem to find
               ys in (F.84a) as a function of y,  and u, since the mapping Pf(y, + ys, u,)  acting onto the
               range of  L is regular. This means that it is possible to express ys as

                                             Ys  = h(Y,, 4).                       (F.85)

               Equation (F.85) is valid only locally, in a neighbourhood of  (0, u,)  with tangency prop-
               erties similar to (F.17), i.e.

                                             =
                                     hfy,, 4) 0,     hdy,, u,)  = 0,               (F.86)
               which means that h is at least second order in yc, h = 61~~)~. obtain the bifurcation
                                                                   To
               equations, we introduce (F.83) into (F.84b) and use (F.85) to find

                                      (1 - P)f(Yc + We, uc), ue) = 0.              (F.87)
               Usually, h(y,, u,)  cannot be found analytically in closed form, but it can be obtained using
               Taylor series in terms of y,  and p = u - u,,  to any desired order. Note that to determine
               (F.87) to  a certain order n, we need to find h(y,, u,)  only to order n  - 1, since h is a
               nonlinear function of y,.  In fact, in many cases, e.g. under certain symmetry conditions,
               it is not necessary to solve (F.84a) to find the bifurcation equation to order n.
                 To  show the reader how  such an  operation can be  carried out, the following simple
               nondimensional system is considered (Troger & Steindl 1991):


                                                                                   (F.88)

               It corresponds to the buckling of a rod under a compressive load u = P/EZ. We  assume
               that  the  rod  is  simply supported at both  ends, i.e.  $'(O)  = @'(l) = 0, and  we  want to
               find the bifurcation equation for the solution $ = 0. The linear operator L is defined by
               taking the (FrCchet) derivative of  (F.88) at $ = 0:

                                                                                   (F.89)


               with  boundary  conditions  ~'(0) = ~'(1) = 0. Solving the  eigenvalue problem  Lx = 0
               leads to the well-known critical parameter u,  = n2, with the corresponding eigenfunction
              B cos(n6).  Consequently,  kerL = span{cos nt}  and  since  L* = L,  dimkerL =
               dimkerL* = 1. The range  of  L is  given  by  the  function g(x)  orthogonal to  the  range
              of L*, i.e. Jd  g(6) cos(nt)d(  = 0.
                 We  can now decompose the image space: to find the projection P onto the range of
              L, we  recall that  for any  function f(c), the projection  (I - P)f((-)  must be  in  kerL*,
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