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Models for  Asphalt Concrete   237


              The initiation and propagation of the crack in the cylindrical specimen under conven-


              tional indirect tensiletest (IDT) are modeled. This study is unique in its consideration of
              material heterogeneity. It allows researchers to link the micro-scale damage with the


              real pavement failure on the global scale.
              7.11.3  Cohesive Zone Model Used in Modeling Fatigue of AC
              Few studies (Song et al., 2005, 2006, 2008; Kim et al, 2006) have been conducted to inves-
              tigate the fatigue of AC. Kim et al. (2006), Kim and Lutif (2008) started to incorporate
              the cohesive zone model into a damage model to explain the mechanism of the AC fa-
              tigue. Kim et al. (2006) developed a computational damage model which is able to ac-
              count for material viscoelasticity, heterogeneity, and path-and rate-dependent energy
              dissipation as cracks initiate and propagate. The model incorporates elastic behavior of
              the aggregate particles, viscoelastic behavior of the asphalt matrix, and time-dependent
              fracture both within the asphalt matrix and along boundaries between matrix and ag-
              gregate particles. Rate-dependent progressive cracking up to failure was implemented
              by incorporation of a cohesive zone fracture model. In the model, the tractions are de-
              scribed in terms of the displacement differences across the cohesive zone. In Kim’s
              study, a nonlinear cohesive zone model developed by Allen and Searcy (2001) was used
              because that model can reflect nonlinear viscoelastic damage growth in the asphalt
              mixtures and predict damage evolution, microcracking, post peak material softening,
              and eventual fracture failure. The equation is shown below:
                                       ut()        t        ∂λ t ()
                                 Tt() =  i  [ −α  t ( )][ ∫  C ( − π )  τ d ]   (7-109)
                                                     CZ
                                            1
                                                       t
                                                              τ
                                  i   λδ                     ∂τ
                                        t ()
                                          i        0
                  where i = n (normal direction), t (tangential direction), or r (radial direction),
                    T i (t) = cohesive zone traction,
                    u i (t) = cohesive zone displacement,
                    l(t) = cohesive zone strain,
                      d i  = cohesive zone material length parameter,
                    a(t) = cohesive zone damage evolution function, and
                  C (t) = linear viscoelastic stress relaxation modulus of cohesive zone
                    CZ
                 The damage evolution function a(t) can be experimentally determined by perform-
              ing small-scale fracture tests. The cohesive zones, which are subjected to damage and
              fracture, are modeled by employing interface elements along the aggregate surface. The
              elements were randomly specified in the sample to maximize the power of the model to
              predict random crack initiation and propagation. The laboratory dynamic frequency
              sweep test and dynamic shear rheometer test are used to determine the viscoelastic
              property parameters in the model. The damage and fracture properties of the cohesive
              zone interfaces were determined by utilizing a tensile fracture test. Damage growth was
              captured by using an optical microscope and analyzed by video.


        7.12  Other Fatigue Studies
              Al-Qadi et al. (2005) discussed thermal fatigue cracking in flexible pavements based on
              experimental results from the Virginia Smart Road. Thermal fatigue is caused by re-
              peated thermal cycles; a finite element simulation model was developed to simulate the
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