scholarly journals The effect of tool wear on the quality of lap joints between 7075 t6 aluminum alloy sheet metal created with the FSW method

2017 ◽  
Vol 20 (1) ◽  
pp. 100-106 ◽  
Author(s):  
Rafał Burek ◽  
Dawid Wydrzyński ◽  
Jarosław Sęp ◽  
Wojciech Więckowski
Keyword(s):  
Aluminum Alloy ◽  
Tool Wear ◽  
Sheet Metal ◽  
Alloy Sheet ◽  
Lap Joints ◽  
Aluminum Alloy Sheet

scholarly journals Process metallurgy design for high-formability aluminum alloy sheet metal generation by using two-scale FEM

2011 ◽  
Vol 10 ◽  
pp. 2250-2255 ◽  
Author(s):  
Hiroyuki Kuramae ◽  
Hidetoshi Sakamoto ◽  
Hideo Morimoto ◽  
Eiji Nakamachi
Keyword(s):  
Aluminum Alloy ◽  
Sheet Metal ◽  
Alloy Sheet ◽  
Aluminum Alloy Sheet ◽  
Process Metallurgy

scholarly journals Forming limit curve determination of AA6061-T6 aluminum alloy sheet

2017 ◽  
Vol 20 (K2) ◽  
pp. 51-60
Author(s):  
Hao Huu Nguyen ◽  
Trung Ngoc Nguyen ◽  
Trung Ngoc Nguyen ◽  
Hoa Cong Vu
Keyword(s):  
Aluminum Alloy ◽  
Constitutive Model ◽  
Sheet Metal ◽  
Damage Model ◽  
Alloy Sheet ◽  
Analytical Models ◽  
Forming Limit ◽  
Aluminum Alloy Sheet ◽  
Limit Curve ◽  
Forming Limit Curve

The forming limit curve (FLC) is used in sheet metal forming analysis to determine the critical strain or stress values at which the sheet metal is failing when it is under the plastic deformation process, e.g. deep drawing process. In this paper, the FLC of the AA6061-T6 aluminum alloy sheet is predicted by using a micro-mechanistic constitutive model. The proposed constitutive model is implemented via a vectorized user-defined material subroutine (VUMAT) and integrated with finite element code in ABAQUS/Explicit software. The mechanical behavior of AA6061-T6 sheet is determined by the tensile tests. The material parameters of damage model are identified based on semi-experience method. To archive the various strain states, the numerical simulation is conducted for the Nakajima test and then the inverse parabolic fit technique that based on ISO 124004-2:2008 standrad is used to extracted the limit strain values. The numerical results are compared with the those of MK, Hill and Swift analytical models.

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