Elements tested
T2D2
T3D2
B21
B31
SAX1
C3D8R
CPE4R
CPS4R
CAX4R
S4R
S4RS
S4RSW
M3D4R
ProductsAbaqus/StandardAbaqus/Explicit Elements testedT2D2 T3D2 B21 B31 SAX1 C3D8R CPE4R CPS4R CAX4R S4R S4RS S4RSW M3D4R Features testedJohnson-Cook plasticity model. Problem descriptionThis verification problem tests single-element models that are run under simple loading conditions (uniaxial tension, uniaxial compression, and simple shear). The purpose of this example is to test the Johnson-Cook plasticity model by comparing it to the Mises plasticity model with equivalent plastic hardening. Figure 1 shows the 26 elements used in the analysis in their original shapes. The elements in the top row are modeled using the Johnson-Cook material model; the elements in the bottom row are modeled using the Mises plasticity model with an equivalent hardening curve. The elastic material properties are Young's modulus = 124 GPa and Poisson's ratio = 0.34. The plastic hardening is chosen to be where is the yield stress (unit in MPa) and is the equivalent plastic strain. The material properties are those of OFHC copper as reported by Johnson and Cook (1985). A plot of versus is shown in Figure 2. Results and discussionResults obtained by using the Johnson-Cook material model are smoother than corresponding results obtained by using the Mises plasticity model. The Johnson-Cook model has an analytical expression for the nonlinear hardening curve; whereas the hardening curve for Mises plasticity model is linear between input data points, as shown in Figure 2. Figure 3 shows the comparison of the stress-strain responses obtained with the Johnson-Cook and the Mises plasticity models using the C3D8R element under uniaxial tension; Figure 4 shows the comparison of the stress-strain responses obtained with the Johnson-Cook and the Mises plasticity models using the CPE4R element under uniaxial compression; Figure 5 shows the comparison of the stress-strain responses obtained with the Johnson-Cook and the Mises plasticity models using the CPE4R element under simple shear. Input filesAbaqus/Standard input files
Abaqus/Explicit input files
References
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