2018
DOI: 10.3390/met8100761
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Application of a GTN Damage Model Predicting the Fracture of 5052-O Aluminum Alloy High-Speed Electromagnetic Impaction

Abstract: An increasing demand exists within the automotive industry to utilize aluminum alloy sheets because of their excellent strength-weight ratio and low emissions, which can improve fuel economy and reduce environmental pollution. High-speed automobile impactions are complicated and highly nonlinear deformation processes. Thus, in this paper, a Gurson-Tvergaard-Needleman (GTN) damage model is used to describe the damage behavior of high-speed electromagnetic impaction to predict the fracture behavior of 5052-O alu… Show more

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Cited by 19 publications
(13 citation statements)
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“…The titanium alloy was used, but the plastic hardening and damage parameters are estimated from the experimental shear curve (see Table 4). With these parameters, the maximum equivalent stress is about σ max = 1340 MPa, and a ductility of ε p max = 0.297 [55,56]. As shown in Figure 8, the coupled material model had fit the experiment value well when equivalent plastic strain less than ε p = 0.21 and the material damage accumulate rapidly to D max = 0.99 when equivalent plastic strain ε p = 0.297.…”
Section: Pure Shear Test Of Titanium Alloy Sheetmentioning
confidence: 88%
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“…The titanium alloy was used, but the plastic hardening and damage parameters are estimated from the experimental shear curve (see Table 4). With these parameters, the maximum equivalent stress is about σ max = 1340 MPa, and a ductility of ε p max = 0.297 [55,56]. As shown in Figure 8, the coupled material model had fit the experiment value well when equivalent plastic strain less than ε p = 0.21 and the material damage accumulate rapidly to D max = 0.99 when equivalent plastic strain ε p = 0.297.…”
Section: Pure Shear Test Of Titanium Alloy Sheetmentioning
confidence: 88%
“…The elastic-plastic and damage parameters of the aluminum alloy (5086) are given in Table 6. The plastic parameters of the material are obtained, from the experimental curves, in which the maximum stress is about σ max = 366 MPa for equivalent plastic strain ε p = 0.17 and then the material stiffness deteriorates to zero when equivalent plastic strain equal to ε p max = 0.27 ( Figure 12) [55,56]. The numerical meshing parameters of the compression test are presented in Table 7.…”
Section: Compression Of Thin Truncated Aluminum Sheet Cylindermentioning
confidence: 99%
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