Forming Limit Stress Diagram Prediction of Aluminum Alloy 5052 Based on GTN Model Parameters Determined by In Situ Tensile Test

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ژورنال

عنوان ژورنال: Chinese Journal of Aeronautics

سال: 2011

ISSN: 1000-9361

DOI: 10.1016/s1000-9361(11)60045-9