Page 452 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
P. 452

424               SLENDER STRUCTURES AND AXIAL FLOW

                      According to the generalization of the Euler-Bernoulli  beam theory, the stress couples
                    Ax, A,, Az in the beam when bent and twisted from the state expressed by  K,,  K:,  to to
                    that expressed by  K, K’,  t* are given by
                                                                    =
                          Ax = EZ(K - K,),   dy = H(K’ - K:),    dZ GJ(t* - to).        (6.30)
                      In the discretization to be introduced later, the pipe is divided into a series of constant
                    curvature elements; i.e. within a given element,

                                                     - 0,                               (6.31)
                                                         =
                                                      as
                    where the number of  elements required will depend on the shape of  the pipe centreline
                    and the accuracy desired.
                      Combining equations (6.2), (6.3) and (6.30) yields




                                                                                         (6.32)
                      Then, substituting equations (6.32) into (6.22) and (6.23), and neglecting the  higher-
                    order terms, one obtains

                                    Qx=-El                                              (6.33)


                                                                                        (6.34)

                      By adding equations (6.19), (6.20) and (6.21) to (6.27), (6.28) and (6.29), respectively,
                    one may obtain the equations of motion of  the system, which no longer depend on the
                    reaction forces R,,  R,  and Rzo between  the  pipe  and  the  fluid. Then,  utilizing equa-
                    tions (6.6), (6.15) and  (6.32)-(6.34) and  neglecting higher  order  terms,  the  governing
                    equations of motion for the dynamical system may be obtained, namely:












                                        a2u
                         +(m+M+M,)-         =o,                                         (6.35)
                                        at2



                                                            +
                                                 +
                                              a2v       a2v     av               a2v
                          - (GYO + Gfyo) + MU  - 2MU - c - + (WZ + M  +Ma)-          = 0,
                                              as2       atas    at               at2
                                                                                         (6.36)
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