Page 468 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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440               SLENDER STRUCTURES AND AXIAL FLOW

                    that  the  critical  flow  velocity  is  also  lower,  reflecting  the  relative  stiffness  in  the  two
                    directions. These results are also very close to Chen’s (1973), except for the second mode
                    in one caset.
                      Before closing this discussion, it is remarked that, throughout this chapter, the modes are
                    numbered  sequentially,  strictly in ascending order of  frequency, irrespective of whether
                    they are asymmetric or symmetric. For in-plane motions of  a semi-circular pipe,  modes
                    1-4  in  Figure 6.5  correspond  respectively  to  the  modes  in  Figure 6.7(a-d),  i.e.  the
                    modes  are numbered in  ascending order  of  the  number  of  nodes.  Similarly, for out-of-
                    plane motions: the first mode would have no nodes, the second mode a node at mid-point,
                    and so on.
























                    Figure 6.7  Schematics of  (a,c) the asymmetric  and (b,d) symmetric modes for in-plane  motions
                        of  an inextensible semi-circular pipe at ii = 0, and approximately for an extensible one.


                    6.4.2  Extensible theory

                    As  in  the  previous  case,  a  study  of  convergence  was  conducted,  to  determine  what  a
                    reasonable number of  finite elements would be for accurate computation of  the eigenfre-
                    quencies.  Some results  are presented  in  Figure 6.8  for U = 0 and  various  values of  d.
                    It  may be  seen that convergence is very  slow, and that it is affected by the  slenderness
                    parameter  d (i.e. ApL2/Z); convergence for the  third  mode is even  slower  (Misra et aE.
                    1988b). For  a  small  number  of  elements  (10 or  so), the  results  for different  values  of
                    d are very different. For a larger number of elements (40 or so), the results are compa-
                    rable. In the curved beam theory used in this work, it has been assumed that the length
                    of  the pipe  is  large  in  comparison  with  its  radius.  This  implies  that  d must  be  large;
                    however, calculations with large d result in high computational cost. Therefore, a value
                    of d that provides a reasonable trade-off between cost and accuracy has been used in the
                    calculations to be presented, namely d = lo4.

                      +In this regard, it is noted  that the value  of ii* at which  w*  = 0 should be independent of  ,9,  as is the case
                    in Chen’s results but not  in those of Misra et al. - either due to a plotting error in the  latter or, more likely,
                    because of  the use of  an insufficient  number of finite elements to ensure adequate accuracy.
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