TY - JOUR
T1 - Forming limit analysis for two-stage forming of 5182-O aluminum sheet with intermediate annealing
AU - Li, Jingjing
AU - Carsley, John E.
AU - Stoughton, Thomas B.
AU - Hector, Louis G.
AU - Hu, S. Jack
N1 - Funding Information:
Financial support for this research was provided through the General Motors Collaborative Research Lab in Advanced Vehicle Manufacturing at The University of Michigan. The authors wish to thank the GM Information Systems and Services for computational resources and technical support.
PY - 2013
Y1 - 2013
N2 - Stress-based forming limit diagrams for a two-stage forming technique with an intermediate annealing step were generated for aluminum alloy 5182-O with a new experimental/theoretical methodology. It was demonstrated that unlike strain-based forming limits, stress-based forming limits are independent of pre-strain levels, pre-strain paths and annealing conditions, and converge to a single forming limit curve that is close to the stress forming limit of the as-received material. For this purpose, AA5182-O specimens were pre-strained to various levels in uniaxial, plane strain, and equibiaxial tension; smaller shapes were extracted, annealed, and tested in limiting dome height (LDH) tests. Strain fields for the forming limit diagrams were measured with stereo digital image correlation during each LDH test, where the onset of localized necking was identified to construct the forming limits. In the calculation of stress-based forming limit curves, only the as-received material properties were required, while the effects of pre-strain and annealing were accounted for with a calculated constant "effective plastic strain." An analytical method is described to develop a new experimental/theoretical methodology effectively predicting the pre-strain and annealing effects. This enables reliable prediction of formability in multi-stage forming processes interrupted by annealing treatment employed to recover additional stretchability in critical areas of a formed part.
AB - Stress-based forming limit diagrams for a two-stage forming technique with an intermediate annealing step were generated for aluminum alloy 5182-O with a new experimental/theoretical methodology. It was demonstrated that unlike strain-based forming limits, stress-based forming limits are independent of pre-strain levels, pre-strain paths and annealing conditions, and converge to a single forming limit curve that is close to the stress forming limit of the as-received material. For this purpose, AA5182-O specimens were pre-strained to various levels in uniaxial, plane strain, and equibiaxial tension; smaller shapes were extracted, annealed, and tested in limiting dome height (LDH) tests. Strain fields for the forming limit diagrams were measured with stereo digital image correlation during each LDH test, where the onset of localized necking was identified to construct the forming limits. In the calculation of stress-based forming limit curves, only the as-received material properties were required, while the effects of pre-strain and annealing were accounted for with a calculated constant "effective plastic strain." An analytical method is described to develop a new experimental/theoretical methodology effectively predicting the pre-strain and annealing effects. This enables reliable prediction of formability in multi-stage forming processes interrupted by annealing treatment employed to recover additional stretchability in critical areas of a formed part.
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U2 - 10.1016/j.ijplas.2012.10.004
DO - 10.1016/j.ijplas.2012.10.004
M3 - Conference article
AN - SCOPUS:84875840183
SN - 0749-6419
VL - 45
SP - 21
EP - 43
JO - International journal of plasticity
JF - International journal of plasticity
T2 - 2012 Plasticity Conference
Y2 - 3 January 2012 through 8 January 2012
ER -