Page 43 - Using ANSYS for Finite Element Analysis A Tutorial for Engineers
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30  •   Using ansys for finite element analysis
                Apply boundary condition:

                   ∧   ∧  ∧    ∧              ∧       ∧
                              u
                                0
                At x = 0  u =  d x ∴ () =  a +  a () =  d x ∴ a =  d x1
                                          0
                           1
                                              1
                                        2
                                                   1
                                     1
                                                      ∧   ∧
                                              ∧
                          ∧
                       ∧
                   ∧
                               ∧
                At x =  L u =  d x ∴ () =  a +  a () =  d x ∴ a =  d x −  d x1
                               uL
                                                       2
                                          L
                           2
                                              2
                                        2
                                     1
                                                        L
                                                   1
                Substituting values of coefficients:
                          ∧   ∧       ∧ x   ∧   ∧ x    ∧    ∧ x  ∧ x    ∧  
                     ∧
                                                        
                                                                   1
                  u ∧   +   d x2  − d x1   x ∧  =  1 −  +    d x  = 1 −    d x  
                                                                
                ∴= d x1                    d x1    2               
                            L         L     L      L  L   ∧
                                                                
                                                          d x   
                                                                   2
                         ∧
                         
                  ∧
                  u
                      N
                         d
                ∴= [] 
                         
                             ∧         ∧ x
                             x
                Where  N =−  L   and  N = L
                          1
                                    2
                        1
                    N  and N  are called shape functions or interpolation functions. They
                           2
                     1
                express the shape of the assumed displacements. The sum of all shape
                functions at any point within an element should be equal to 1.
                       N  = 1      N  = 0    at node 1
                                    2
                         1
                       N  = 0      N  = 1    at node 2
                                    2
                         1
                       N  + N  = 1
                             2
                         1
                   N 1                              N 2    N 1        N 2
                 1                2  1                 2  1              2
                                                                L
                         L                   L
                Step 3: Define the strain/displacement and stress/strain relationships
                                              ∧
                                          ∧
                                    ∧
                              ∧
                Deformation,   d = () − ()= d x2  − d x1
                                L
                              u
                                    u 0
                                                         ∧
                                                             ∧
                From the force/deformation relationship:  Tk= d = kd x −  d x   
                                                        
                                                          2
                                                        
                                                             1
                Where T is the tensile force and δ is the total elongation.
                Step 4: Derive the element stiffness matrix and equations
                Consider the equilibrium of forces for the spring.
                          ∧         ∧  ∧  
                At node 1,  f 1 =− T =  kd x −  d x  
                                  
                           x
                                        2
                                    1
                                  
                          ∧         ∧  ∧ 
                At node 2,  f  =  T =  kd x −  d x 
                          2 x        2  1  
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