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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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Problem 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 value10/10 subtests passed (uniaxial, pure shear, hydrostatic invariance, Bauschinger reverse yield, multilinear, tangent FD)
Our result10/10 subtests passedmax relative error 0.000000%
Deviation0%
Tolerance5%
StatusPASS · 0%
Mesh detailsНабор 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

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