Page 554 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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524               SLENDER STRUCTURES AND AXIAL FLOW

                    The derivatives &,,/as,  &,/as,  aezo/as may be found by the same principle as those of
                    a rotating vector. Thus, &,,/as  = S2  x e,  = +,ezo  + toeyo, where G? = Koe,  + .;eyo  +
                    toe,,;  and similarly for the others. Then, using (J.l), one obtains




                      Combining equations (J.6)-(J.8)  with  (J.9), the  components of  the  fluid acceleration
                    vector given in equations (6.15) may be obtained.


                    J.4  THE EQUATIONS OF MOTION FOR THE PIPE
                    Consider an infinitesimal element of the pipe contained between the cross-section through
                    PI and Pi  on the strained centreline, and the forces and moments acting on it, as shown
                    in Figure J.l. Qxo, Qyo  and Qzo  are components, referred to the  (x0, yo, zo) frame, of  the
                    resultant of the transverse shear forces Q,,  Qy and Q:  = Q, +A,p,  [see equation (6.18)];
                    Axe, hyo and A,,  are the components of the resultant of the bending moments Ax, Ay
                    and the twist couple A, in the XO, yo  and zo  directions; F,,  F,  and F,  are the compo-
                    nents, referred to the (&  y&  ,&)  frame [defined in Figure J.l(b)]  of the force resultant at
                    Pc  per unit  Iength of  the centreline, which includes the inertial and gravity forces, the
                    viscous damping and pressure forces associated with the surrounding fluid and the reac-
                    tion force associated with the internal flow; Oxo, 0, and O,,  are components, referred
                    to the (xb, y;, zb)  frame of the moment resultant at Pt per unit length, which include the
                    moments of rotatory inertia and external moments, if  any.
                      We  next  consider  an  inertial  coordinate  frame  (XO, YO, ZO), relative  to  which  the
                    (xo, yo, zo) and (x&  y&  26) frames have direction cosines It and ZTj',  such that, for instance,
                    Qyo  along YO is given by lr2Qx0 + Eit2QyO  + 1;2Qz0. In the limit of 6s -+ 0, l:j  = It'.  After
                    projecting all forces and moments in Figure J.l(b) on the inertial frame (XO, Yo, Zo) with
                    the aid of diagrams such as Figure 5.2,  and balancing forces and moments along Xu, Yo
                    and ZO, one obtains
                              a
                                [ZTiQxo  + l;iQyo  + l;~Qzo] + lilFxo + E;lFyo  + /;IFzo = 0,
                              a
                              - [GQxo + G2Qyo  + l3*2Qzo]  + 1;2Fq + l&Fyo  + l3*2FZO = 0,   (J. 10:
                              as
                              a
                              - ['?3QXo  + '&QYO  + %Qz0]  + ly3Fxo + l;3Fy0 + 13*3Fz0 = 0,
                              as
                            a
                            -
                            as  [l;i&xo  + l&JGo  + GiAzO] + 12  (173Q,W  + Z&Qm  + l&Q,>
                              - 13  (%Qq + l&.7Qy0  + Z&Q,)   + (lyl@,,  + Z$lOyo + I* 31 O  ) = 0,
                            a
                            - [lLdh~ + G2Ayo +K&Azo] + 13  (l;lQxo  + l;iQN  + l;lQzo)
                            as
                              - '1  (';3   QxO  + Z;3Qyo  + Z3*3QZO)  + (1;2@xo  + 1z2Oyo + /3*2074) = 0,  (J.11)
                            a
                            - [G'/uxg + 1$3 &yo  + 13*3dzo] + !I  (&Qq + l&QyO  + l&Qz0)
                            as
                              - 12 (ZTiQxo  + I&Qyo  + l;lQQ) + (l;30x0 + Z&OyO + Z;30zo) 0,
                                                                                  =
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