Quantifying Formability during Two-Stage Forming of Aerospace Alloys using Hosford-Coulomb Ductile Damage Model Framework
摘要
The present study investigates the formability behavior of Inconel 718 (IN718) sheets during single-stage (SHET) and two-stage hole-expansion (THET) tests. For THET experiments, 8% equi-biaxial pre-strain was imparted in the first stage of deformation. The anisotropic Barlat Yld89 material model was used in the finite element (FE) modeling of SHET and THET tests. Moreover, the calibrated Hosford-Coulomb (HC) advanced ductile damage model-based fracture forming limit diagram (FFLD) in the principal strain (