Page 341 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 341

328                      Introduction to the Finite Element Method   Chap. 10





                                                           i;/2-

                                                                 @   Figure  10.7-1.
                              Solution:  We  use  a single element  (D -  (D  and first determine  the  inverse of the stiffness
                                  matrix.  Beeause  r,  = 0 ,  =0,  the  stiffness equation  from  Eq.  (10.2-1) is
                                                                12 - 6/,
                                                            El
                                                               - 6/,  4/r

                                  Its  inverse,  using the  adjoint  method,  is
                                                               1  4/r  6/,
                                                          El  12/r
                                       The equivalent  hnite element  forees,  from  Eq.  (10.7-4),  are

                                   F^  =   p4)y{x) dx =                                  “ 31^^
                                                                         ' 1/2
                                                            -1              88   .
                                   M2 =   f '  -  P<f>4iOI\d^  =  - p l \ i '   { - f -   +  ^ ^ ) d ^   =
                                       M/2                 •'1/2            1536
                                       J \  /I
                                                           d \  /I
                                  Substituting these values  into  the  inverted  equation, we  have
                                                                    J_3
                                                         4/f      -   32^/,
                                                                    Ï
                                                    \2El  6/,   12  88   I
                                                                  1536
                                                        '   52   528   ^      (     \
                                                    pit  ^  32   1536          5.125
                                                    \2EI    78    1056    48 E/  7.000
                                                           32/,  ^ 1536/,

                                  These  results  agree with  those  ealeulated  from  the  area-moment  method.


                        10.8  GENERALIZED FORCE PROPORTIONAL
                            TO DISPLACEMENT

                              When  the  generalized  force  is  proportional  to  the  displacement,  it  can  be  trans­
                              ferred  to  the  left  side  of  the  equation  of  motion  to  combine  with  the  stiffness
                              matrix  for  the  free  vibration.  Presented  in  this  section  are  two  cases:  (1)  for
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