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                       Fracture Mechanisms in Nonmetals                                            291


                       6.3 CONCRETE AND ROCK

                       Although concrete and rock are often considered brittle, they are actually quasi-brittle materials
                       that are tougher than most of the so-called advanced ceramics. In fact, much of the research on
                       toughening mechanisms in ceramics is aimed at trying to make ceramic composites behave more
                       like concrete.
                          Concrete and rock derive their toughness from subcritical cracking that precedes ultimate
                       failure. This subcritical damage results in a nonlinear stress-strain response and R-curve behavior.
                          A traditional strength-of-materials approach to designing with concrete has proved inadequate
                       because the fracture strength is often size dependent [50]. This size dependence is due to the fact
                       that nonlinear deformation in these materials is caused by subcritical cracking rather than plasticity.
                       Initial attempts to apply fracture mechanics to concrete were unsuccessful because these early
                       approaches were based on linear elastic fracture mechanics (LEFM) and failed to take account of
                       the process zones that form in front of macroscopic cracks.
                          This section gives a brief overview of the mechanisms and models of fracture in concrete and
                       rock. Although most of the experimental and analytical work has been directed at concrete as
                       opposed to rock, due to the obvious technological importance of the former, rock and concrete
                       behave in a similar manner. The remainder of this section will refer primarily to concrete, with the
                       implicit understanding that most observations and models also apply to geologic materials.
                          Figure 6.39 schematically illustrates the formation of a fracture process zone in concrete,
                       together with two idealizations of the process zone. Microcracks form ahead of a macroscopic
                       crack, which consists of a bridged zone directly behind the tip and a traction-free zone further
                       behind the tip. The bridging is a result of the weak interface between the aggregates and the matrix.
                       Recall Section 6.2.4, where it was stated that fiber bridging, which occurs when the fiber-matrix
                       bonds are weak, is the most effective toughening mechanism in ceramic composites. The process
                       zone can be modeled as a region of strain softening (Figure 6.40(b)) or as a longer crack that is
                       subject to closure tractions (Figure 6.40(c)). The latter is a slight modification to the Dugdale-
                       Barenblatt strip-yield model.
                          Figure 6.40 illustrates the typical tensile response of concrete. After a small degree of nonlin-
                       earity caused by microcracking, the material reaches its tensile strength σ  and then strain softens.
                                                                                  t
                       Once σ  is reached, the subsequent damage is concentrated in a local fracture zone. Virtually all
                             t
                       of the displacement following the maximum stress is due to the damage zone. Note that Figure 6.40
                       shows a schematic stress-displacement curve rather than a stress-strain curve. The latter is inap-
                       propriate because nominal strain measured over the entire specimen is a function of gage length.
                          There are a number of models for fracture in concrete, but the one that is most widely referenced
                       is the so-called fictitious crack model of Hillerborg [51, 52]. This model, which has also been called
                       a cohesive zone model, is merely an application of the Dugdale-Barenblatt approach. The Hillerborg
                       model assumes that the stress displacement behavior (σ-δ ) observed in the damage zone of a tensile
                       specimen is a material property. Figure 6.41(a) shows a schematic stress-displacement curve, and
                       6.41(b) illustrates the idealization of the damage zone ahead of a growing crack.
                          At the tip of the traction-free crack, the damage zone reaches a critical displacement δ . The
                                                                                                 c
                       tractions are zero at this point, but are equal to the tensile strength σ , at the tip of the damage zone
                                                                             t
                       (Figure 6.39(c)). Assuming that the closure stress  σ and opening displacement  δ are uniquely
                       related, the critical energy release rate for crack growth is given by

                                                                 d
                                                         G = ∫  c δ  σδ                          (6.25)
                                                          c
                                                              0
                       which is virtually identical to Equation (3.43) and Equation (6.22).
                          The key assumption of the Hillerborg model that the  σ-δ relationship is a unique material
                       property is not strictly correct in most cases because process zones produced during the fracture
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