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F inite Element Method and Boundar y Element Method   263


              of virtual work. The spatial discretization of the weak form equations uses finite ele-
              ment and some spatial interpolation scheme for the displacement u, i.e.:
                                               u =  Nu q                         (8-62)

                        q
                 Where u  is the displacement at the nodes, N is the interpolating function. Through
              the strain-displacement relation and constitutive model, the equilibrium equation
              could be represented as a set of equations with node displacements as independent
              variables, or:
                                                 q
                                              gu () = 0
                                                                                 (8-63)
                 For a quasi-static initial boundary value problem in a specific time interval, the
              solution of Equation (8-63) is obtained incrementally and successively by dividing the
              time interval into an appropriate number of time steps. For each step, the solution
              procedure for a displacement driving FE system could be summarized as the follow-
              ing three steps:

                 1. Global computation (equilibrium equations). Under the defined material
                    behavior, loading condition, kinematic conditions, Equation (8-63) could be
                    solved iteratively. For example, for the FE code ABAQUS, Newton’s method is
                    used. Using Δu, the strain increment Δe can be obtained.
                 2. Local computation (constitutive equations). At each material calculation point,
                    stress and the set of internal state variables are integrated and updated under
                    specified initial conditions and given strain increment Δe. For ABAQUS and
                    user’s materials, this is accomplished through UMAT. The following sections
                    deal with this computation.
                 3. Residual force computation and convergence check. Determine the residual
                    stress of the FE equilibrium equations and check convergence condition. If not
                    reached, repeat 1 and 2.

                 Two basic strategies exist for the step 1 and 2 computations: (1) simultaneous solu-
              tion of the equilibrium and constitutive equations, or (2) separate solution of the two
              sets of equations requiring iteration procedures at the global level. Among the tech-
              niques of the first type, the method by Kanchi et al. (1978) and Marques et al. (1983) and
              the method by Hughes et al. (1985) are two different possibilities. The technique by
              Kanchi and Marques evaluates state variables at time t k+1  by Taylor series expansion at
              time t k  without further iteration, while the technique by Hughes uses Newton-Raphson
              iterations. Among the techniques of the second type, there are two techniques also: (a)
              use the same time step for both equilibrium and constitutive equations (Snyder et al.,
              1981; Heaps et al., 1986) and (b) use different time steps for equilibrium and constitutive
              equations with smaller time steps for constitutive equations (Ottosen and Gunneskov
              1985). Most of these techniques could be applied to local computations.
                 In local computations, FE solution could be treated as the following mathematical
              equivalency:

                 Given at Step k: state variables, s k  and Δe, Δt, t k
                 Find at Step k+1: state variables and Δs,  σ k+1 = σ + Δ σ t  k+1  =  t + Δ t
                                                               ,
                                                         k
                                                                     k
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