Forming Limit Stress Diagram Prediction of Aluminum Alloy 5052 Based on GTN Model Parameters Determined by In Situ Tensile Test
Tensile Test、In Situ、Model、Based、Aluminum Alloy
24
V25;TM2
Aeronautical Science Foundation of China 03H53048
2011-12-06(万方平台首次上网日期,不代表论文的发表时间)
共9页
378-386