Issue 38

R. Fincato et alii, Frattura ed Integrità Strutturale, 38 (2016) 231-236; DOI: 10.3221/IGF-ESIS.38.31 235 Figure 3: Reference elements in the central cross section. Figure 4: Damage contour field before crack opening (axial strain = 0.1670). Figure 5: Damage contour field at the crack opening (axial strain = 0.1675). Figure 6: Damage contour field at the end of computation (axial strain = 0.1756). Figure 7: Material calibration parameter. Figure 8: Applied load vs nominal axial strain. Figure 9: Stress triaxiality in the reference elements in Fig. 3. Figure 10: H evolution in the reference elements in Fig. 3.