Page 203 - Handbook of Materials Failure Analysis
P. 203

5 Case Study    199






                                        M
                                          total








                                           M                  I
                                             tower

                                                   EI







                  FIGURE 8.4
                  Tank modeled mechanically as a single mass supported by a tower.



                  geometrical characteristics of the structure (dimensions of the tank), the relation uses
                  the flexional rigidity (EI), and the weight distribution of the structure (P).These are
                  two missing parameters in the empirical relation proposed in the Algerian
                  seismic code.
                     The rigidity K 0 of the supporting system is deduced by:
                                             4π 2  g   3   EI
                                          2               K 0
                                              T 2  P   l 3  M total
                                         ω ¼    ¼       ¼                        (8.9)
                                                    0
                  Then,
                                                           3   EI
                                                 M total
                                                                                (8.10)
                                                  33        l
                                        K 0 ¼                3
                                            M total +    M tower
                                                 140
                  The calculation of the stiffness is given in the Table 8.6.
                  5.3.4 Calculation of eigenpulsations
                  The equilibrium equations can be formulated in a matrix form by the following
                  equation:
                                                                                (8.11)
                                                           f
                                       f f i tðÞg + f a tðÞg + f e tðÞg ¼ ftðÞg
                                                    f
                                             f
                                                                       €

                                                          f
                     The vector of inertial forces can be written as f i tðÞg ¼ M½Š   XtðÞ
   198   199   200   201   202   203   204   205   206   207   208