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3.2  Finite Element Method                                 43



                                 Since the strain is related to the displacement and deflection as,
                                                             u          2 w
                                                                    z
                                                      x
                                                              x         x   2
                                 Then, the stress can be determined from the deflection as,
                                                                     2 w
                                                        x        Ez  x   2

                                            For  a  typical  beam  in  a  three-dimensional  frame
                                 structure,  its  deflection  may  be  in  a  direction  other  than  the  z-
                                 coordinate.  In addition, the beam may be twisted by torsion caused
                                 by  the  applied  loads  or  affected  by  other  members.    These
                                 influences must be considered and included for the analysis of three
                                 dimensional beam structures.


                                 3.2   Finite Element Method

                                     3.2.1  Finite Element Equations
                                            Finite  element  equations  can  be  derived  directly  from
                                 the  beam  governing  differential  equation  by  using  the  method  of
                                 weighted  residuals.    Detailed  derivation  can  be  found  in  many
                                 finite  element  textbooks  including  the  one  written  by  the  same
                                 author.   The derived finite element equations are in the form,
                                                                
                                                        K 
                                                                     F
                                                                             
                                 where   is  the  element  stiffness  matrix;   is the element
                                        K
                                 vector  containing  nodal  unknowns  of  deflections  and  slopes;  and
                                   is  the  element  vector  containing  nodal  forces  and  moments.
                                  F
                                 These element matrices depend on the selected beam element types
                                 as explained in the following section.

                                     3.2.2  Element Types
                                           The  basic  beam  bending  element  with  two  nodes  is
                                 shown  in  the  figure.    Each  node  has  two  unknowns  of  the
                                 deflection  w  and slope  .
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