plasticity_analyze_static_fem
Run static linear-elastic FEA on a selected solid to check stress and displacement under defined supports and loads, using isotropic or orthotropic material data.
Instructions
Run bounded linear-elastic CalculiX analyses for one selected native Solid, modeled as one material and one print process; never combine material datasets. The default isotropic model uses youngsModulusMPa and poissonRatio with exact matching evidence. A process-matched uniaxial coupon may supply the isotropic Young's modulus only; use plasticity_match_material_coupon_data first and bind only an unambiguous exact-process record. Poisson ratio always needs separate evidence.
To use an orthotropic model, pass orthotropicMaterial. In that mode youngsModulusMPa is E1 and poissonRatio is nu12; orthotropicMaterial supplies E2, E3, nu13, nu23, G12, G13 and G23. When the immutable exact-process coupon record contains the measured full tensor and nu12, bind it with orthotropicMaterial.couponRecordId and process, and set materialCoupon to the same record ID/process. The server checks E1, nu12, all seven remaining constants, each evidence object and the confirmed print frame against that record before solving and again when the saved report is read. Otherwise, provide separate exact-value evidence for every property. Measured/sourced evidence requires URL, SHA-256 and locator; assumptions require an explicit derivation and remain scenario-only. The server rejects an unstable normal-compliance matrix and non-positive moduli. Give axis1DirectionGlobal, axis2ReferenceDirectionGlobal, and buildDirectionGlobal in the global CAD frame. The build direction must be explicitly user-confirmed or sourced, and material axis 3 must align with it; axis 3 is the layer-normal direction. Axis 1 and 2 are orthogonalized into a right-handed local frame; zero or parallel axes are rejected. Without layerPlanePlan, this is one homogeneous frame. For a per-layer orientation analysis, pass a complete layerPlanePlan made from the exact single-material process and G-code: profile hash and measured layer height must match orthotropicMaterial.process; the plan must include every layer (up to 256), confirmed slicer-to-CAD and coupon-road-axis mappings, and complete planar road-direction evidence for every layer. Linear deposition and XY circular arcs are integrated for I/J offsets and signed R radii. P multi-turn arcs, malformed or mixed arc forms, non-XY arc planes, absolute I/J center mode, and G5/G5.1 splines or G5.2/G5.3 NURBS blocks remain incomplete. The server cuts the STEP B-Rep at the planned interfaces before meshing, verifies each face-to-surface fragment by exact plane/bounds/area evidence, and assigns each conformal volume region the same measured tensor with that layer's mapped frame. The report marks these components as layer-local. Static FEA treats the interfaces as perfectly bonded; it does not predict delamination or interlayer failure. Use the separate cohesive-interface analysis with measured interface tests for that. Varying layer frames cannot use directional component allowables expressed in one fixed material frame. Orthotropic analyses do not accept a von Mises allowable because it is not a qualified orthotropic failure criterion. The screen checks no multiaxial interaction and is diagnostic only; it is not a failure verdict, strengthPass or print approval. Without all nine supported directional limits, no orthotropic stress screen is returned.
For an optional measured 3D Tsai-Wu screen, bind one qualified single-material print record by supplying its ID as orthotropicMaterial.tsaiWuQualificationRecordId together with orthotropicMaterial.process. The server resolves the immutable record only when it is the unique exact match for printer, filament, profile hash, orientation, infill percentage and pattern, wall loops, top/bottom shell layers, nozzle temperature and measured slicer layer height, and checks that its measured print axes match the FEA material frame. It loads the nine un-factored X/Y/Z tensile/compressive and XY/XZ/YZ shear failure strengths plus three normalized XY/XZ/YZ normal-interaction coefficients and their source evidence from that record; agents do not copy these values manually. Each strength evidence entry must attest testAxis and testMode in the confirmed material frame; each biaxial interaction and its source dependencies must attest its corresponding plane. Legacy records without directional metadata remain readable but cannot be bound to Tsai-Wu FEA. Alternatively, provide the complete inline orthotropicMaterial.tsaiWuCriterion with process-matched, direction-qualified evidence. The interaction matrix must be positive definite. CalculiX evaluates the full material-local tensor at each integration point and reports the maximum failure index and proportional load factor to index one per case and mesh. This diagnostic first-failure surface never establishes whole-part strength or print approval. It assumes one homogeneous material and does not resolve individual roads, discrete layer delamination, nonlinear response, fatigue, buckling or convergence; without measured data it is omitted.
For isotropic analyses only, an optional factoredVonMisesAllowableMPa requires directly measured/sourced matching evidence with URL, SHA-256, locator and factoredVonMisesAllowableBasis. The allowable must already include design factors and apply to this material/process; do not convert a generic datasheet strength or raw coupon peak into an allowable. Its comparison with sampled mesh peaks is diagnostic only and never establishes strength, convergence, strengthPass or print approval.
Choose either legacy supportFaceIds (all three global translations fixed on each planar face) or 1–8 explicit supportConditions; each condition fixes only its listed global translation axes x/y/z to zero at every node on that face. Ask the user to confirm the actual restraints; do not infer them from a photo or face orientation. Before solving, the tool checks that mapped support-node translations remove all six rigid-body translations and rotations; this is only a restraint-rank check and does not prove elastic stability or physical support validity. It has no friction, contact or rotational support model. Provide either legacy single-case loads or up to eight named independent loadCases. Each case may combine uniform face tractions in N/mm² and resultant face loads with force N, application point mm and free moment N·mm. Resultant-load points must lie on their selected planar faces; free moments use a balanced equivalent nodal couple over that face. Optionally request one to three mesh refinement steps, each halving meshSizeMm; the job count is bounded to 12. Cases at the same mesh level are compared only when Gmsh reproduces an identical mesh byte for byte. Each case reports sampled trends for raw maximum von Mises stress and observed displacement (increasing, decreasing, unchanged, non-monotonic, or insufficient-levels), plus raw peak-locator centroid shifts. These are diagnostics only, never a convergence pass, strength pass or print approval.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| bodyId | Yes | ||
| revision | Yes | ||
| faceLoads | No | ||
| loadCases | No | ||
| meshSizeMm | Yes | ||
| poissonRatio | Yes | ||
| layerPlanePlan | No | ||
| materialCoupon | No | ||
| resultantLoads | No | ||
| supportFaceIds | No | ||
| youngsModulusMPa | Yes | ||
| supportConditions | No | ||
| meshRefinementSteps | No | ||
| orthotropicMaterial | No | ||
| poissonRatioEvidence | Yes | ||
| youngsModulusEvidence | No | ||
| factoredVonMisesAllowableMPa | No | ||
| factoredVonMisesAllowableBasis | No | ||
| factoredVonMisesAllowableEvidence | No |