Page 219 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 219

206                              Properties of Vibrating Systems   Chap. 6

                                  If the system is started from zero displacement and an arbitrary distribution of velocity
                                  ^ (0),  determine  the coefficients  ^4,  and
                              6-41  Figure P6-41  shows a shaft supported by a bearing that has translational and rotational
                                  flexibility.  Show  that  the  left  side  of  the  shaft  flexibility  Eq.  (6.1-1)  or  (6.1-2)  of
                                  Example 6.1-4 should  now be  replaced  by
                                                                V
                                                              d - p
                                  From  the  relationship  between  rj,p,y,6,  and  loads  P  and  M,  determine  the  new
                                  flexibility equation













                                                                     Figure P6-41.
                              6-42  Set up the matrix equation of motion for the  3-DOF  system of Fig.  P6-18  in terms of
                                  stiffness. Transform  it  to the standard eigen-problem form, where  A  is symmetric.
                              6-43  In  Example  6.10-1  for  the  forced  vibration  of  a  10-story  building,  the  equation  of
                                  motion  for the first  mode was given  as
                                                     /I. ;   + 0.02235-^1  =  -1.2672«o(0
                                               +  0.299
                                  Assume  the values  yjk/m  =  3.0  and  ¿'j  =  0.10,  and  solve  for  the  time  response  using
                                  RUNGA when  the ground  acceleration  is given by Fig.  P6-43.
















                            /  0 0.1 0.2  0.3 04 0.5  0.6  0.7  0.8 0.9 1.0 1.2
                          f{t)  0 1.0 0-0.7 0 0.5  0-0.3  0 0.2 0  0  Figure P6-43.
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