Page 187 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 187

174                               Properties of Vibrating Systems   Chap. 6

                                  moment method/  the deflection  at the various stations is equal to the moment of the
                                  M/EI  area  about  the  position  in  question.  For  example,  the  value  of  iZ2i  ^ ^12
                                  found from Fig.  6.1-3  as  follov/s:
                                                            1           11 i i
                                                           ^ 2 (2 /rx   3
                                                        £7               3  El
                                  The other values (determined as before) are

                                                      - U l L           n i l
                                                      ~  3  El   “21  “  ‘   3  El
                                                        8                2.5  /3
                                                                    l
                                                   "22 ~  3  El  (I'yri  —  C  3  El
                                                      -  ill           - Ill
                                                   “33   3  El  “i3  “  “31  -   3  El
                                  The  flexibility matrix can  now be written  as

                                                           P  27  14   4
                                                          3 El  14  8  2.5
                                                               4   2.5  1
                                  and the symmetry about  the  diagonal should be  noted.
                             Example 6.1-4
                                  The  flexibility influence  coefficients can  be  used  to  set  up  the  equations  of a flexible
                                  shaft supported by a rigid bearing at one end with a force P  and a moment  M at the
                                  other end,  as shown  in  Fig.  6.1-4.





                                                                         Figure 6.1-4.

                                      The deflection  and slope  at the  free  end  is
                                                          y  =    -f-
                                                                                          (6 .1-1)
                                                          6 = a2\P +
                                  which can be expressed by the  matrix equation
                                                        yi  ^  r«ii   «12]  i P
                                                        o f -   [«21  «22j\M              ( 6.1-2)
                                  The  influence coefficients in  this equation  are
                                                    P               P          J _
                                               «11   3£/-   «12   «21   2E r    El        (6.1-3)

                                  E.  P.  Popov,  Introduction  to  Mechanics  of Solids  (Englewood  Cliffs,  NJ:  Prentice-Hall,  1968),
                             p.  411.
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