摘要
运用SHPB实验研究超高强度钢30CrMnSiNi2A在应变率500-5000s^-1时的应力应变关系,并对典型试样进行了金相观察.实验得到30CrMnSiNi2A钢的屈服强度随着应变率的增加从1655MPa增加到1908MPa.基于试样金相和断口分析,30CrMnSiNi2A钢在高应变率冲击加载条件下产生了韧窝型沿晶断裂,导致材料宏观上表现为剪切破坏.结合准静态实验数据,确定了30CrMnSiNi2A钢的Johnson-Cook本构模型的材料参数.
As an outstanding performance aviation material, the understanding of dynamic behavior of ultrahigh strength steel 30CrMnSiNi2A at high strain rates is of importance in a range of applications. The curves of stress and strain in different strain rates (500-5 000 s^-1) of 30CrMnSiNi2A steel are obtained with split Hopkinson pressure bar(SHPB) experiments, and the micro-deformation characters were observed by metallography. The results indicate that 30CrMnSiNi2A steel is sensible of strain rate, and dynamic compression leads to shear failure with the angle 45°. The yield stress increases from 1 655 MPa to 1 908 MPa with increasing strainrate (500 - 5 000 s^-1). Through metallographic analyses, the failure is found to be dimple intercrystalline fracture under high strain-rate loading. Meanwhile, the material parameters of Johnson-Cook model are determined through the SHPB experiments and quasi-static results.
出处
《北京理工大学学报》
EI
CAS
CSCD
北大核心
2010年第3期258-262,共5页
Transactions of Beijing Institute of Technology
基金
国家自然科学基金资助项目(10802009)
国家重点实验室基金资助项目(ZDKT08-04)