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IntroductIon to FInIte element AnAlysIs   •   37
                      Example 2
                      Derive a finite element to solve this problem.


                                         2



                                              1



                                                      1000 lb
                                              60°
                                       3    2
                                                              1000 lb
                                             30°      1
                                                 3
                                       4


                                             L

                          To derive this problem must be tack the rotational effect by multiply-
                      ing the local stiffness matrix in rotational matrix (R).
                          The rotational matrix in this problem can be derived as:


                                           c 2  cs  −c 2  − 
                                                           cs
                                                 2         2 
                                         =   cs  s  −cs  −s   
                                          
                                           −c 2  −cs  c 2  cs  
                                                 2         2  
                                           −cs  −s   cs   s  

                      Where: c  = cos  (β), s  = sin  (β), cs = cos (β)*sin (β).
                                   2
                             2
                                             2
                                        2
                      β = The angle between x-axis and the element C.C.W.
                                              c 2       cs         s 2
                               β = 120°    0.25     −0.433      0.75
                                1
                               β = 180°    1        0           0
                                2
                               β = 210°    0.75     0.433       0.25
                                3
                          The  property  of this  matrix  is a symmetric  matrix. This matrix is
                        multiplied with the local stiffness matrix of each element.

                                               EA
                                                     i []
                                          k  i ()  =  ii  Ri = 12
                                                          ,,3
                                                L i
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