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51 2  Matrix methods of structural analysis



                            -  12J/~~                                           SYM
                             -12~~1~~ 12~~1~~
                               6p/L2     -6X/L2      4/L
                   [Kg] = EI
                                                   -6p/~2
                              -12p2/~3  12~~1~~ 12p2/~3
                              12~~1~~ -12~~1~~ 6x1~~ -12~~1~~ 12~~1~~
                            -  6p/L2     -6X/L2      2/L      6p/L2     6X/L2   4XIL
                                                                                   (12.47)

                 Again the stiffness matrix for the complete structure is assembled from the member
                 stiffness matrices,  the  boundary  conditions  are  applied  and  the  resulting set  of
                 equations solved for the unknown nodal displacements and forces.
                   The internal shear forces and bending moments in a beam may be obtained in terms
                 of the calculated nodal displacements. Thus, for a beam joining nodes i andj we shall
                 have obtained the unknown values of vi, Bi and vi, 0,.  The nodal forces Fy,i and Mi are
                 then obtained from Eq. (12.44) if the beam is aligned with the x axis. Hence







                 Similar expressions are obtained for the forces at nodej. From Fig. 12.6 we see that
                 the shear force S,  and bending moment M in the beam are given by

                                                                                   (12.49)

                 Substituting Eqs (12.48) into Eqs (12.49) and expressing in matrix form yields

                                  12          6           12          6
                                            --          --
                                              L2         L3                        (12.50)
                                                                   6
                   {2}=E'[12z  -x  - - 6    6    4  -- 12 x+- 6  --      2
                               L3    L2  -zx+z L3           L2    L2X+Z
                   The matrix analysis of the beam in Fig.  12.6 is based on the condition that no
                 external forces are applied between the nodes. Obviously in a practical case a beam
                 supports  a  variety  of  loads  along  its  length  and  therefore  such beams  must  be
                 idealized into a number of beam-elements for which the above condition holds. The
                 idealization is accomplished by merely specifying nodes at points along the beam
                 such that any element lying between adjacent nodes cames, at the most, a uniform
                 shear and a linearly varying bending moment. For example, the beam of  Fig.  12.7
                 would  be  idealized into  beam-elements  1-2, 2-3  and  3-4 for which  the unknown
                 nodal displacements are v2, S2,  03, v4 and 0,  (q =   = v3 = 0).
                   Beams supporting distributed loads require special treatment in that the distributed
                 load is replaced by a series of statically equivalent point loads at a selected number of
                 nodes. Clearly the greater the number of nodes chosen, the more accurate but more
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