Abstract:In order to study the dynamic mechanical property and constitutive relation of 2024-T42 aluminum alloy under medium-low strain rate, quasi-static and medium-low strain rates tests were carried out by using a quasi-static tensile test system and INSTRON VHS160-100/20 high velocity test system to obtain the stress-strain curves at different strain rates.Considering the effect of necking on the true stress-strain, a simulation inversion method was used to correct the true stress-strain curve after necking, which was then fitted based on the Johnson-Cook constitutive model.The results show that the rate sensitivity of 2024-T42 aluminum alloy is weak in the intermediate and low strain rate range, but it has a strong strain hardening effect; the inversion correction method based on simulation analysis can better reconstruct the true stress-strain curve after necking point; and through the aluminum tube crush test and simulation analysis, the rationality of the inversion correction method and the accuracy of the obtained constitutive model parameters are verified.
[1] 刘继华,李荻,郭宝兰,等.LC4高强铝合金的慢应变速率拉伸实验[J].材料科学与工艺,2001,9(1):37-41.
LIU Ji-hua, LI Di, GUO Bao-lan, et al. Slow strain rate tension test of high-strength aluminum alloy[J]. Materials Science and Technology, 2001,9(1):37-41.
[2] 惠旭龙,白春玉,葛宇静,等.2A16铝合金中应变率力学性能研究[J].振动与冲击,2017,36(19):66-70.
HUI Xu-long, BAI Chun-yu,GE Yu-jing, et al. Dynamic properties of 2A16 aluminum alloy under intermediate strain rate[J]. Journal of Vibration and Shock, 2017,36(19):66-70.
[3] 刘军,杨黎明,谢书港,等.6061铝合金的动态拉伸性能及其本构模型[J].机械工程材料,2017,41(3):49-53.
LIU Jun, YANG Li-ming, XIE Shu-xiang, et al. Dynamic tensile properties and constitutive model of 6061 aluminum alloy[J]. Material for Mechanical Engineering, 2017,41(3):49-53.
[4] 谢灿军,童明波,刘富,等.7075-T6铝合金动态力学实验及本构模型研究[J].振动与冲击,2014,33(18):110-114.
XIE Can-jun, TONG Ming-bo, LIU Fu, et al. Dynamic tests and constitutive model for 7075-T6 aluminum alloy[J]. Journal of Vibration and Shock, 2014,33(18):110-114.
[5] 陈俊岭,舒文雅,李金威. Q235钢材在不同应变率下力学性能的实验研究[J]. 同济大学学报(自然科学版),2016,44(7),1071-1075.
CHEN Jun-ling, SHU Wen-ya, LI Jin-wei. Experimental study on dynamic mechanical property of Q235 steel at different strain rates[J]. Journal of TONGJI University(Natural Science), 2016,44(7),1071-1075.
[6] Lee W S, Su W C, Li C F. The strain rate and temperature dependence of the dynamic impact properties of 7075 aluminum alloy[J]. Journal of Materials Processing Technology, 2000,100(1):116-122.
[7] ZHANG Yi-ben, YAO Song, HONG Xiang, et al. A modified Johnson-Cook model for 7N01 aluminum alloy under dynamic condition[J]. Journal of Central South University, 2017, 24(11):2550-2555.
[8] 李娜,李玉龙,郭伟国. 3种铝合金材料动态性能及其温度相关性对比研究[J]. 航空学报, 2008,29(4):903-908.
LI Na, LI Yu-long, GUO Wei-guo. Comparision of mechanical properties and their temperature dependence for three aluminum alloys under dynamic load[J]. Acta Aeronautica et Astronautica Sinica, 2008,29(4):903-908.
[9] 谢灿军,童明波,刘富,等. 民用飞机平尾前缘鸟撞数值分析及实验验证[J]. 振动与冲击, 2015,34(14):172-178.
XIE Can-jun, TONG Ming-bo, LIU Fu, et al. Numerical analysis and experimental verification of bird impact on civil aircraft's horizontal tail wing leading edge[J]. Journal of Vibration and Shock. 2015,34(14):172-178.
[10] 高倩倩,胡本润,杨伟. 应变速率对2024铝合金拉伸性能的影响研究[J]. 热加工工艺,2014,43(12):113-116.
GAO Qian-qian, HU Ben-run, YANG Wei. Effect of strain rate on mechanical properties of 2024 alloy[J]. Hot Working Technology, 2014,43(12):113-116.
[11] 郭伟国,田宏伟. 几种典型铝合金应变率敏感性及其塑性流动本构模型[J]. 中国有色金属学报,2009,19(1):56-61.
GUO Wei-guo, TIAN Hong-wei. Strain rate sensitivity and constitutive models of several typical aluminum alloys[J]. The Chinese Journal of Nonferrous Metals, 2009,19(1):56-61.
[12] 刘富,张嘉振,童明波,等. 2024-T3铝合金动力学实验及其平板鸟撞动态响应分析[J]. 振动与冲击,2014,33(4):113-118.
LIU Fu, ZHANG Jia-zhen, TONG Ming-bo, et al. Dynamic tests and bird impact dynamic response analysis for a 2024-T3 aluminum alloy plate[J]. Journal of Vibration and Shock. 2014,33(4):113-118.
[13] 王雷,李玉龙,索涛,等. 航空常用铝合金动态拉伸力学性能探究[J].航空材料学报,2013,33(4):71-77.
WANG Lei, LI Yu-long, SUO Tao, et al. Mechanical behavior of commonly used aeronautical aluminum alloys under dynamic tension[J]. Journal of Aeronautical Materials. 2013,33(4):71-77.
[14] 张正礼. 2024铝合金动态力学本构模型构建[J]. 沈阳航空航天大学学报,2014,31(2):47-50.
ZHANG Zheng-li. Construction of dynamic mechanical constitutive model of 2024 aluminum[J].Journal of Shenyang Aerospace University.2014,31(2):47-50.
[15] 白春玉,刘小川,周苏枫,等. 中应变率下材料动态拉伸关键参数测试方法[J].爆炸与冲击,2015,35(4):507-512.
BAI Chun-yu, LIU Xiao-chuan, ZHOU Su-feng, et al. Material key parameters measurement method in the dynamic tensile testing at intermediate strain rate[J]. Explosion and Shock Waves.2015,35(4):507-512.
[16] JOHNSON G R, COOK W H. A constitutive model and data for metals subjected to large strains, high strain rates and high temperatures[C]. Proceeding of the 7th International Symposium on Ballistics. 1983:541-547.
[17] Merdan B, Sven D W, Markus F, et al. An extension of the GISSMO damage model based on lode angle dependence[C]. LS-DYNA anwender forum, Bamberg 2010.
[18] 李宏烨,庄新村,赵震. 材料常用流动应力模型研究[J]. 模具技术,2009,5:1-4.
LI Hong-ye, ZHUANG Xin-cun, ZHAO Zheng.Study on flow stress models commomly used in materials[J].Die and Mould Technology.2009,5:1-4.
[19] KANG W J, CHO S S, HUH H, et al. Modified Johnson-Cook model for vehical body crashworthiness simulation[J]. International Journal of Vehicle Design. 1999,21:424-435.
[20] COWPER G R, SYMONDS P S. Strain hardening and strain rate effects in the impact loading of cantilever beams[J]. Small Business Economics. 1957,31(3):235-263.
[21] HUH H, KANG W J, HAN S S. A tension split Hopkinson bar for investigating the dynamic behavior of sheet metals[J]. Experimental Mechanics. 2002,42(1):8-17.