Page 60 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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CONCEPTS, DEFINITIONS AND METHODS                    43

              It should also be noted that in cases of symmetric confinement of the fluid, this term may
              entirely vanish.

               IC) Magnitude considerations: wide and narrow annuli
               By re-writing expressions (2.120a,b) in terms of R;/R,, and taking the limit (R;/R,) -+ 0,
               i.e. as the outer cylinder radius becomes essentially infinite, one obtains

                                                                                 (2.133a)

               and
                                     F,,,,; = 0,   as   (R;/R,) -+ 0.            (2.133b)
               Equation (2.133a) for  n = 1 yields the  result just  obtained in  (2.131) in  another way,
               that  the  added mass  for R, +. 00  is  equal  to  the  ‘displaced’ mass  of  fluid. Also,  the
              physically reasonable result is obtained in equation (2.133b) that, for an infinitely distant
               outer cylinder, the effect of  accelerations of  the inner one is infinitely faint.
                 In the other limit, writing R,  = R; + h and R; Y R,  2: R, and taking h to be small,


                                                                                  (2.134)

              This expression shows that for thin shells, and also for light, hollow cylinders in narrow
               annuli,  the  added  mass  can  easily  exceed and  be  several times  larger than  the  struc-
               tural mass; i.e. M’ >>  M  in  (2.126), for instance. Expression (2.134) would suggest that
               the  added  mass  becomes  infinitely  large as  h -+ 0.  This  is  not  so,  however, because
               the Stokes number becomes small before that  limit is reached, signalling that  the limit
               of  applicability of  inviscid  theory  has  been  surpassed; for  oscillations of  the  shell or
              cylinder  of  amplitude Eh  and  frequency w, where  E  is  a small number, the  Stokes (or
               oscillatory Reynolds) number is B = cwhR/u  ew(h/R)R2/v. An  alternative, and more
               general, pertinent Stokes number is B = wlt2/u. In either case, it is clear that as h + 0, or
               h/R -+ 0 and E  < 1, B becomes sufficiently small for viscous effects not to be negligible
               (see Section 2.2.3). Furthermore, in  addition to  the  added  damping, the  forces  associ-
               ated with shell motions become extremely large, as seen from (2.134), due to the very
               large  accelerations  in  the  narrow  fluid  annulus; hence, sustained oscillation  under  the
              circumstances does not occur.
                 It  is  finally noted  in  (2.120a,b), (2.133a) and  (2.134) that  the  added mass becomes
               smaller as  n  is  increased, which  is  reasonable in  physical  terms: the  hills and  valleys
               associated with deformation of  the shell are half a circumference apart for n = 1, while
              they are much closer for large n; hence the fluid accelerations are correspondingly smaller
              for the larger n, and so is the added mass.

               (dl Fluid coupling and the added mass matrix
              If both shells are flexible, the only thing that changes in the formulation is that boundary
              condition  (2.1 15b) needs  to  take  a  form similar to  (2.1 15a). Recalling the meaning of
              influence coefficients in solid mechanics, by analogy (and as already done in the foregoing)
              one can think of  a force on the inner shell due to nth  mode motion of  the inner shell,
              F;,n;, or of  a force on the inner shell due to motion of the outer one, F;,,,,  and so on.
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