Formability of TWIP (twinning induced plasticity) automotive sheets

被引:131
作者
Chung, Kwansoo [1 ]
Ahn, Kanghwan [1 ]
Yoo, Dong-Hoon [1 ]
Chung, Kyung-Hwan [2 ]
Seo, Min-Hong [2 ]
Park, Sung-Ho [2 ]
机构
[1] Seoul Natl Univ, Res Inst Adv Mat, Dept Mat Sci & Engn, Seoul 151742, South Korea
[2] POSCO Tech Res Labs, Gwangyang Si 545090, Jeonnam, South Korea
关键词
TWIP steel; Sheet metal forming; Formability; FLD; Yld2000-2d; ANISOTROPIC YIELD FUNCTIONS; KINEMATIC HARDENING LAWS; SPRING-BACK EVALUATION; AUSTENITIC STEEL; DUCTILE FRACTURE; STRAIN-RATE; PREDICTION; METALS; FORMULATION; BEHAVIOR;
D O I
10.1016/j.ijplas.2010.03.006
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The main objective of this work is to experimentally and numerically evaluate the macro-performance of the automotive TWIP (twinning induced plasticity) sheet in conjunction with formability. In order to characterize the mechanical properties, the simple tension and compression tests were performed for anisotropic properties, while the strain rate test was carried out to evaluate strain rate sensitivity. The forming limit diagram was measured and incorporated into the simulation program, while the theoretical prediction of the diffuse and localized necking was also carried out utilizing Hill's and the M-K theories as well as Dorn's and Swift's diffuse theories. Note that the generalized criteria of Hill's, Dorn's and Swift's theories were derived for general anisotropic sheets as well in this work. For numerical simulations, the anisotropic yield functions Yld2000-2d and Hill48 as well as the isotropic Mises yield function were selectively applied along with the isotropic hardening law. Formability verification was performed, utilizing Yld2000-2d, for the hemispherical dome stretching, notch and simple tension tests with specimens selectively prepared by milling and punching, while anisotropic properties were verified through the three point bending and cylindrical cup drawing tests, comparing the performance of the three yield functions. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:52 / 81
页数:30
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