Page 285 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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266               SLENDER STRUCTURES AND AXIAL FLOW

                    is very similar to the case of internal flow; as this is discussed in Chapter 8 (Volume 2),
                    it will not be duplicated here.
                      An alternative method is to obtain the eigenvalues and eigenfunctions {A;, x;(()}  of the
                    conservative part of (4.80), q””  + u2q” + ij = 0, as well as those of its adjoint, [A;,  +;($)};
                    these are in fact the same as for problem (2.52), and are given by equations (2.59). Then,
                    introducing   xj(()q;  (t) into  equation (4.80)  and  using  the  biorthogonality  relation
                    (2.57), another form of equation (4.81) is obtained, in which  [MI and [K] are diagonal.
                    The presence  of  the Coriolis term  in  (4.80), however, means that  [C] is  not  diagonal.
                    Hence, even more than for the problem in  Section 2.1.6, this method offers no special
                    advantage, since it cannot diagonalize the nonhomogeneous problem  ‘in one step’ as it
                    would if  this were an ordinary mechanical system.
                      Let us now turn our attention to the forced response of  a cantilevered pipe with a tip
                    point muss, A, subjected to an arbitrary force field, f(e, t). The dimensionless equations
                    of  motion and boundary conditions in this case are

                                   q””  + u2q” + 2purj’ + a?j + ij  = f((, t);          (4.85a)

                                   q(0) = q’(0) = 0,   q”(1) = q”’(1) - pij(1) = 0,     (4.85b)
                    where p = A/[(M + m)L]. An alternative way of  formulating the problem leads to

                                 q”” + u2q” + 2/9’/*U?j’ + a?j + [l + WUs(6 - 1)lij = f((, t).   (4.86a)
                                 q(0) = q’(0) = 0,   q”(1) = q”’(1) = 0,                (4.86b)
                    in which Us((  - 1) is the Dirac delta function. As hinted in Section 2.1.4,  the decoupling
                    of  the  equations  in  this  case  poses  some  interesting  problems,  because  the  boundary
                    conditions in (4.85a,b) are time-dependent. Three possible procedures immediately spring
                    to mind, as follows:
                      Method (a): to utilize the eigenfunctions +;(e) of the problem q’”’  + ij  = 0 subject to
                    boundary conditions (4.85b) to discretize the system;
                      Method (b): to utilize these same eigenfunctions +;(()  but apply them to an ‘expanded
                    domain’ of the problem (Friedman 1956), which effectively means that the time-dependent
                    boundary conditions are added to the equation of  motion, so that one obtains








                      Method (c): to utilize the cantilever beam eigenfunctions, 4; (e), directly to decouple
                    equation (4.86a).
                      In  principle, one can show directly which  of  these methods are correct or otherwise,
                    but  here  we  shall  do  so  by  means  of  sample  computations. To  simplify matters  and
                    since the main point of  interest is  the decoupling procedure, we consider the homoge-
                    neous undamped version of  this system: f((, t) = 0, a = 0. The results are presented in
                    Table 4.6, for two-mode discretization in all cases. For the same value of  p, the values
                    of  WI and w2  for u = 0 are the same whether B = 0 or   = 0.1, and hence they are not
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