Page 262 - The Combined Finite-Discrete Element Method
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DISCRETE CRACK MODEL      245








                                             s
                                                         2b
                                               2a
                                                    s






                         Figure 7.13 A thin plate with a crack parallel to the edges.


           operations). However, such meshes, when coupled with the combined single and smeared
           crack model, result in stress and strain fields in the vicinity of the crack tip being inaccurate
           by an order of magnitude. Thus, the resulting fracture patterns are extremely sensitive
           to the local element size and element orientation. With over one billion elements, it is
           feasible that some real scale bench blasting problems can be accurately modelled using
           the combined smeared and discrete crack model as described in this chapter.
             The theoretical conclusions about mesh sensitivity are best demonstrated through a set
           of numerical experiments designed to look at the influence of the element size on fracture
           results. A finite size thin plate with a crack parallel to the edges subjected to uniform
           inner pressure employed for this purpose is given in Figure 7.13.
             The geometry of the plate is defined by:

                                            a = 10 mm
                                                                                (7.28)
                                            b = 30 mm

           while the following material properties are assumed:

                                Modulus of Elasticity E = 26.6GPa
                                      Poisson’s ratio ν = 0.205
                                                                                (7.29)
                                     Tensile strength f t = 5MPa

                                            Density ρ = 2340 kg/m 3

           The load is increasing with time:

                                        σ = 20,000t MPa                         (7.30)
           where t is time in seconds and σ is the uniform pressure on crack walls.
             The problem is solved for two different energy release rates (G f = 2γ = 3N/m and
           G f = 2γ = 30 N/m), each time using four different element sizes, meshes A, B, C and
           D, as shown in Figure 7.14. Mesh A is characterised by an element size of h = 10 mm.
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