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98     CHAPTER 5 Failure analysis of reinforced concrete structures




                         in which E and G are longitudinal and transversal elasticity modules, respectively,
                         and ε and γ are normal and distortional strains, respectively.

                         2.2 PLASTICITY MODEL FOR STEEL

                         Steel, as most part of ductile materials, presents elastic mechanical behavior until
                         reaching its yield stress. After this stress level, there are some movements in the
                         internal crystals of the material, which give it a new strength capacity. In this phase,
                         named hardening, there is loss of stiffness, but the material still has strength capacity
                         until its failure limit. The models based on elastoplasticity theory are appropriate to
                         describe such mechanical behavior. Thus, the model chosen to describe the mechan-
                         ical behavior of reinforcements’ steel is composed by an elastoplastic constitutive
                         law with positive isotropic hardening. The criterion used to verify the elastoplastic
                         steel behavior is given by:
                                                    f ¼ σ s   σ sy + Kψ                  (5.8)

                         in which σ s indicates the steel reinforcements’ layer stress, σ sy is the steel yielding
                         stress, K is the hardening plastic modulus, and ψ is the equivalent plastic strain
                         measurement.
                            The stress over each reinforcement layer is determined as follows:
                                                     f   0 ! σ ¼ Eε
                                                     f > 0 ! σ ¼ E t ε                   (5.9)
                                                                                     EK
                         in which E t is the tangent elastoplastic modulus, which is given by: E t ¼  =  .
                                                                                       ð E + KÞ
                         3 GEOMETRIC NONLINEARITY

                         Figure 5.2 illustrates the initial and final configurations for a given point P, which
                         belong to a solid, after loading action. The horizontal and vertical displacements
                         of such point are defined by:
                                                  u p x, yÞ ¼ uxðÞ y sin θðÞ
                                                   ð
                                                                                        (5.10)
                                                 v p x, yð  Þ ¼ vxðÞ y + ycos θðÞ
                                                                                         0
                         Considering a second-order approximation for displacements, where sin θðÞ ¼ v xðÞ
                                        0 2
                                          x
                                       v ðÞ
                         and cos θðÞ ¼ 1   , Equation 5.10 is rewritten as follows:
                                         2
                                                                0
                                                   u p x, yÞ ¼ uxðÞ yv xðÞ
                                                    ð
                                                                0  2  !
                                                               v xðÞ                    (5.11)
                                                 v p x, yð  Þ ¼ vxðÞ y
                                                                 2
                         in which u and v correspond, respectively, to horizontal and vertical displacement
                         fields for any point along the body.
                            Considering that geometric nonlinearity second-order terms are given by Green
                         strain measurement, the normal and distortional strain fields, ε xx and γ xy , respec-
                         tively, are written as follows:
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