Determination of Johnson-Cook Plasticity Model Parameters for Inconel718

被引:50
|
作者
Farahani, H. K. [1 ]
Ketabchi, M. [1 ]
Zangeneh, Sh. [2 ]
机构
[1] Amirkabir Univ Technol, Min & Met Engn Dept, Tehran, Iran
[2] Razi Univ, Dept Mat Sci & Engn, Kermanshah, Iran
关键词
foreign object damage; impact (ballistic); Inconel718; Johnson-Cook plasticity model; FOREIGN-OBJECT DAMAGE; FRACTURE CHARACTERISTICS; DYNAMIC-BEHAVIOR; CRACK-GROWTH; STRAIN-RATE; FATIGUE; STEEL;
D O I
10.1007/s11665-017-2990-2
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In order to simulate foreign object damage (FOD) phenomenon in aircraft high-pressure compressor blades made of a nickel-based super-alloy, Johnson-Cook (J-C) plasticity model was used. For prediction of material's plastic behavior at temperature of 400 degrees C (working temperature of the blades) in the range of strain rates associated with the FOD phenomenon (in order of 106 s(-1)), material parameters of A, B, C, n and m for the J-C plasticity model had to be determined experimentally. Parameters of A, B and n with values of 1108, 699 MPa and 0.5189, respectively, were obtained from quasi-static tensile tests. Moreover, m was determined to be 1.2861, also through quasi-static tensile tests with a strain rate of 1 s(-1) at three temperatures of 475, 550 and 625 degrees C. However, in order to determine C, firstly a steel ball was impacted on the surface of a flat specimen made of a precipitation-hardening alloy, and then, the impact site was 3D scanned to obtain the induced crater profile. Finally, the impact test (ballistic) was simulated using Abaqus, and a C value of 0.0085 was determined by comparing the actual crater profile with the one obtained from the simulation through a trial-and-error approach.
引用
收藏
页码:5284 / 5293
页数:10
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