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Modeling the strain localization of shell elements subjected to combined stretch–bend loads: Application on automotive sheet metal stamping simulations
This study presents a modeling approach for predicting strain localization during sheet metal stamping processes focused on automotive engineering applications. The so-called stretching-to-bending ratio, ρ, is proposed to characterize the loading conditions acting on an element during stamping proce...
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Published in: | Thin-walled structures 2023-07, Vol.188, p.110804, Article 110804 |
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Main Authors: | , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | This study presents a modeling approach for predicting strain localization during sheet metal stamping processes focused on automotive engineering applications. The so-called stretching-to-bending ratio, ρ, is proposed to characterize the loading conditions acting on an element during stamping processes. Then, localized strain or necking strain is suggested to be a function of ρ. Different stretch–bending tests with different tool radii, i.e., R3, R6, R10, and R50 are conducted for two automotive sheet metals, DP800 and AA6010, to identify their forming limits under combined stretch–bend loads. The calibrated necking limit curve of the AA6016 sheet is then employed in AutoForm R10 software to predict the necking and failure of a stamped panel. Agreement with the experimental observation of failure positions of the panel validates the usefulness of the proposed modeling approach in practice.
•Proposal of the so-called stretching-to-bending ratio, ρ of shell elements•Proposal of the necking limit curve as a function of ρ•Calibrate the necking limit curve of two automotive sheet metals: DP800 and AA6016.•Validate the calibrated AA6016 curve via a test die stamping simulation in AutoForm•Good agreement with experimental observation on the deformed panel’s failure positions. |
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ISSN: | 0263-8231 1879-3223 1879-3223 |
DOI: | 10.1016/j.tws.2023.110804 |