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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Published in | International journal of mechanical sciences Vol. 43; no. 2; pp. 471 - 486 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Oxford
Elsevier Ltd
01.02.2001
Elsevier |
Subjects | |
Online Access | Get full text |
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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. |
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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 |