Determination of ductile damage behaviors of high strain rate compression deformation for Ti-6Al-4V alloy using experimental-numerical combined approach. (September 2018)

• Record Type: Journal Article
• Authors: Chen, Guang; Ren, Chengzu; Lu, Lianpeng; Ke, Zhihong; Qin, Xuda; Ge, Xiang
• Is Part Of: Engineering fracture mechanics. Volume 200(2018)
• Page Start: 499
• Page End: 520
• Publication Date: 2018-09
• Subjects: Failure initial strain -- Ti-6Al-4V alloy -- High strain rate -- Ductile damage -- SHPB tests; Fracture mechanics -- Periodicals; Rupture, Mécanique de la -- Périodiques; Fracture mechanics; Periodicals; 620.112605
• DOI: 10.1016/j.engfracmech.2018.08.020
• Languages: English
• ISSNs: 0013-7944

Abstract

Highlights: Damage occurred at high strain rate and low temperature in Ti-6Al-4V SHPB tests. Damage parameter was determined by measured FIS and SHPB simulation without damage. A coupling JCM plastic and energy density based damage model were presented. Damage behaviors were further validated at higher temperature (T ≥ 300 °C) conditions. Energy density method was effective to keep the flow stress of damage evolution. Abstract: Ductile damage behavior of Ti-6Al-4V alloy was characterized by the evolution of flow curves and deformed specimens in compression tests at high strain rates and various temperatures. Cracks along the shear bands of deformed specimens were observed at lower temperatures (20 °C and 100 °C) and high strain rates (2500–10, 000 s −1 ). The failure initial strains (FIS) during crack generation were calculated according to the measured flow stresses at the transition from stable plastic to damage evolution stage. Special emphasis is placed on the influence of strain rate and temperature on the ductile failure initiation. The failure initiation parameters of Johnson-Cook (JC) damage model were obtained by genetic algorithm (GA) optimization using a combined experimental–numerical approach. That is, the ductile damage parameters were optimized according to the measured FIS and the simulated stress triaxiality, equivalent strains, stresses and temperatures, using compression simulation without damage model. At lower temperatures (T < 300 °C), the failure parameters were used to simulate the flow stresses and deformation of specimen by the JC plastic and damage models. To further validate the failure parameters, at higher temperatures (T ≥ 300 °C), a coupling modified JC (JCM) plastic and energy density based damage model was proposed to characterize the flow curves at damage evolution stage by compression simulation using a subroutine program. The predicted flow stresses and the deformed specimens were consistent with the experimental results.