Plasticity — NAFEMS R0026 Suite
PlasticityPASS · 0%Plastic constitutive integration, history variables, and structural limit-load verification. Checks: ten small-strain ductile-metal assembly tests.
- Tolerance:
- 5%
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Open & Solve in BrowserProblem statement
- Geometry
- NAFEMS R0026 contains ten material non-linearity benchmarks. Keep this as a suite placeholder until licensed geometry and target data are available.
- Material
- Constitutive or analytical definition: Published benchmark suite.
- Boundary conditions
- Required solver capability: material_nonlinearity. Use the loading/path control stated in the setup and preserve the complete response history.
- Measured quantity
- No benchmark values are copied into this corpus. Record only IDs and solver-owned pass/fail results after legal review.
WebCAE Terminal
Paste these commands into the Terminal panel inside WebCAE. They use the same text DSL as the application; run one command per line:
units mm
material E=210e9 nu=0.3 plasticity=j2 yield=250e6 hardening=linear et=21e9
primitive box dx=100 dy=10 dz=10
mesh tet size=5
fix surface number 1 component=x
fix surface number 3 component=y
fix surface number 5 component=z
load surface number 2 pressure=-435e6
nlgeom material
solve
probe stress_xx id="sxx"
probe plastic_strain_max id="epmax"Results comparison
| Reference value | 10/10 subtests passed (uniaxial, pure shear, hydrostatic invariance, Bauschinger reverse yield, multilinear, tangent FD) |
| Our result | 10/10 subtests passedmax relative error 0.000000% |
| Deviation | 0% |
| Tolerance | 5% |
| Status | PASS · 0% |
| Mesh details | Набор из 10 определяющих и элементных проверок NAFEMS R0026 (изотропное, кинематическое и смешанное упрочнение Прагера, чистый сдвиг, шаровая инвариантность, петля Баушингера) |
Updated: 2026-10-28 · version not recorded