Prediction of forming limit diagrams for AL6111-T4 under non-proportional loading

In this paper, an anisotropic damage model for predicting FLDs is extended to predict the sheet metal formability under non-proportional loading involving changing directions of principal strain plane and damage plane. The material chosen for the prediction of FLDs is AL6111-T4 aluminum alloy. A sat...

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Bibliographic Details
Published inInternational journal of mechanical sciences Vol. 43; no. 2; pp. 471 - 486
Main Authors Chow, C.L., Yu, L.G., Tai, W.H., Demeri, M.Y.
Format Journal Article
LanguageEnglish
Published Oxford Elsevier Ltd 01.02.2001
Elsevier
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Summary:In this paper, an anisotropic damage model for predicting FLDs is extended to predict the sheet metal formability under non-proportional loading involving changing directions of principal strain plane and damage plane. The material chosen for the prediction of FLDs is AL6111-T4 aluminum alloy. A satisfactory agreement between the model predictions and test results has been achieved.
Bibliography:ObjectType-Article-2
SourceType-Scholarly Journals-1
ObjectType-Feature-1
content type line 23
ISSN:0020-7403
1879-2162
DOI:10.1016/S0020-7403(99)00123-X