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OneCAD-Simulation/docs/parity.md
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40f98f0af9 Implicit solver: fem kernels (tet4/10, hex8, hex20), sparse Cholesky, block Lanczos, solve.* commands (M4) (#23)
* Renumber the layer table for solver crates: fem at L1, solver at L2, fsi at L3

L0 model -> L1 geometry, mesh, fem, decks, render -> L2 solver (explicit, lbm later)
-> L3 fsi (later) -> L4 doc -> L5 io -> L6 engine -> L7 ui-egui, mcp -> apps.
UI_MIN_LAYER moves to 7, the testkit sits above it.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* modelcraft-fem: element kernels for tet4, tet10, hex8 (full, incompatible modes), hex20 (full, reduced)

Shape functions, Gauss and conical-product quadrature, stiffness, consistent and HRZ-lumped
mass, body forces, consistent pressure loads on faces, integration-point stresses and their
least-squares extrapolation to nodes, isotropic and orthotropic elasticity. The element table is
one row per kind, so wedges, shells and beams are added locally.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* modelcraft-solver: linear static and frequency analysis with an analytic verification suite

Assembly from the resolved model on the node graph, boundary conditions by elimination,
consistent pressure, gravity and body-force loads, nested-dissection ordering, sparse up-looking
Cholesky with a factor-size cap, reactions, integration-point and nodal-averaged stresses, von
Mises; shift-invert block Lanczos with full reorthogonalization for natural modes, participation
and effective mass. ADR 0001 records the own-linear-algebra decision (determinism, wasm).

Verified against closed forms: displacement and traction patch tests for every element, cantilever
tip deflection (Timoshenko) with convergence rates, Lamé cylinder, Kirsch hole (Kt -> 3),
cantilever and free-free beam frequencies with six rigid-body modes.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* Engine: solve.static, solve.frequency and solve.probe; results kept in the session

Results are stored per step, restored on a failed command and cleared when the model changes.
Caps (degrees of freedom, factor entries, Lanczos vectors) may only be lowered; hostile parameters
are tested against a solvable session.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* docs: implicit solver architecture, roadmap M4, parity and references

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* Simplify the solver: shared face integration, block assembly, cached extrapolation

- model: one face integrator (nodal::face_normal_weights) for tractions and pressures
- fem: mid-side tables from ElementKind::edges, orthotropic via inverse3, symmetric
  accumulation without a symmetrize pass, incompatible-mode recovery without K_uu, model's
  coordinate check, dead table rows removed
- solver: one pattern search per node pair (block, scalar and diagonal adds), extrapolation built
  once per element type, reactions from the prescribed rows only, matrices dropped after
  restriction, the free-body shift keyed on the factorization error, step selection in the solver,
  Error::Element naming the element
- engine: the solver owns the default step and the shift check; the model comparison runs once

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

* docs: results are stamped with the session revision

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm

---------

Co-authored-by: jyviko <2501648+jyviko@users.noreply.github.com>
Co-authored-by: Claude Opus 5.5 <noreply@anthropic.com>
2026-10-13 17:44:21 -04:00

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# Capability checklist (reference: Abaqus/CAE)
What an analyst does in a full CAE pre-processor, grouped by milestone, with ModelCraft's status.
Scope comes from the public documentation of Abaqus/CAE and public analyst discussion,
described in our own words; nothing was taken from the product itself (AGENTS.md: no commercial
products are run, no documentation text is copied). Status: **done**, **started**, **planned**.
**HEX** marks items centred on hexahedral meshing, the core goal.
## Where we aim to be better
| # | Opportunity | Why analysts want it | ModelCraft approach |
|---|---|---|---|
| 1 | Hex meshes without manual partitioning | Partitioning a part into sweepable cells by hand is the most cited chore | Sweep and mapped meshing with automatic decomposition that proposes SolidCraft splits (M5); octree all-hex for anything else (M6) |
| 2 | Undo, redo, replay, crash recovery | No general undo; replay files are hard to reuse; corrupted model files | Every action is a journalled command with rollback, undo and redo; autosave with recovery after a crash |
| 3 | Sets that survive changes | Sets and loads break when geometry regenerates or is remeshed | Sets bind to SolidCraft's persistent face, edge and body names and resolve after meshing (M3) |
| 4 | An API that is not a bundled scripting runtime | Version breakage, slow scripts, geometry picked by position | JSON commands over CLI, control channel and MCP |
| 5 | Located diagnostics | Generic error messages | Errors name the element, face or keyword; `mesh.quality` lists failing elements |
| 6 | Lossless deck round trip | Unsupported keywords dropped on import | Deck readers keep unknown keywords and write them back (M9) |
| 7 | Safe, diffable model files | Binary model databases that corrupt or lock to a version | `.modelcraft`: text, line-diffable definition and journal, checksummed binary mesh, versioned format tag, atomic saves with backup, autosave (M3, done) |
| 8 | Geometry checked before meshing | Slivers and tiny faces fail late | Surface preparation reports defects with their location (M1) |
| 9 | No size caps, any solver | Node limits in learning editions; one solver per tool | Free, open source, three deck formats |
| 10 | Clear step history | Loads and BCs propagate between steps implicitly | An explicit step × load/BC table (M3) |
## Checklist
| Area | Capability | Milestone | HEX | Status |
|---|---|---|---|---|
| Geometry | Open SolidCraft designs, bodies, persistent face names, assemblies placed | M1 | | done |
| Geometry | Face-tagged mesh import (3MF) | M1 | | done |
| Geometry | Weld, closed/manifold/orientation and self-intersection checks, feature edges | M1 | yes | started |
| Geometry | Partitions and datums as SolidCraft features (split body/face, construction planes) | M5 | yes | planned |
| Geometry | Midsurface extraction for shells | M8 | | planned |
| Mesh | Size field: global, per face and edge seeds, bias, curvature and proximity refinement | M2 | yes | planned |
| Mesh | Free tet meshing (tet4, tet10 with mid-side nodes on the geometry) | M2 | | started |
| Mesh | Quality metrics, certified validity, verify per set | M1–M2 | yes | done (metrics, gate) |
| Mesh | 2D quad meshing of faces | M5 | yes | planned |
| Mesh | Mapped hex of six-sided regions | M5 | yes | planned |
| Mesh | Sweep hex (extrusions, revolutions) | M5 | yes | planned |
| Mesh | Automatic decomposition into sweepable and mappable regions | M5 | yes | planned |
| Mesh | Conforming interfaces, tet–hex transition with pyramids | M5 | yes | planned |
| Mesh | Octree/grid-dual all-hex for any part | M6 | yes | planned |
| Mesh | Hex-dominant by recombination; polycube | M6 | yes | planned |
| Mesh | Smoothing, untangling, boundary padding, layers through thin walls | M6 | yes | planned |
| Mesh | Mesh editing (move, merge, split, collapse, remesh region), imported orphan meshes | M6 | yes | started (node/element add/remove) |
| Model | Sets and surfaces bound to geometry names | M3 | yes | done |
| Model | Materials: elastic (isotropic, orthotropic), density, unit-system check | M3 | | done |
| Model | Materials: plasticity, hyperelasticity, damage, thermal | M8 | | planned |
| Model | Sections: solid, shell, beam profiles; assignment by set | M3 | | done |
| Model | Composite layups, material orientations, continuum shells | M8 | yes | planned |
| Model | Element formulation per region (integration, incompatible modes, hybrid) mapped per solver | M3 | yes | done (model; per-solver mapping with the deck writers) |
| Model | Boundary conditions: fixed, displacement, symmetry | M3 | | done |
| Model | Loads: force and moment, pressure, gravity, body force | M3 | | done |
| Model | Reference points, kinematic and distributing coupling | M3 | | done |
| Model | Steps: linear static, frequency; output presets | M3 | | done |
| Model | Steps: nonlinear static, explicit dynamics, heat transfer; amplitudes | M7–M8 | | planned |
| Interaction | Tie between non-matching meshes | M7 | | planned |
| Interaction | Contact (general and pairs), friction, automatic pair detection | M7 | | planned |
| Interaction | Bolt pretension, springs, point masses, connectors | M7 | | planned |
| Decks | Abaqus input writer (`deck.write`, flat deck; reports what Abaqus cannot express) | M3 | | done |
| Decks | Nastran bulk data writer (`deck.write`, SOL 101 or 103 per deck; reports what Nastran cannot express) | M3 | | done |
| Decks | LS-DYNA keyword writer (implicit; explicit in M8) | M3 | | done (implicit static and eigenvalue; beam sections planned) |
| Decks | Readers keeping unknown keywords | M9 | | planned |
| Solve | Own linear static and modal solver, verified against analytic solutions | M4 | yes | started (solid elements: tet4, tet10, hex8, hex20) |
| Results | Deformed shape, contours, mode shapes, probes, reaction sums | M4 | | started (results in the session, `solve.probe`, reaction sums; display planned) |
| Results | XY and path plots, cuts, display groups, free-body forces, animation | M9 | | planned |
| Results | Readers for public result formats (Nastran OP2, LS-DYNA d3plot, Abaqus `.fil`) | M9 | | planned |
| Results | Mesh convergence studies | M9 | | planned |
| App | Desktop viewport, model tree, commands, control channel | continuous | | done |
| App | Undo/redo on the command journal, autosave, `.modelcraft` file | M3 | | done |
| App | MCP server, browser build | continuous | | planned |
## Deck notes for the writers
- Node order: the model stores Abaqus/VTK order. Nastran orders the mid-side nodes of 20-node hexes
and 15-node wedges differently; LS-DYNA takes tets and wedges as degenerate hexes and triangles
as degenerate quads. Every mapping is tested by the sign of the element Jacobian after writing.
- Each format's field widths, continuation rules, number forms and label limits are respected by
the writer and checked by golden-file tests on our own examples.
- Abaqus: the model's node order and face numbers are Abaqus's, so connectivity passes through;
element types come from the element kind, the section and its formulation (table in
`crates/decks/src/abaqus.rs`). The step table is bridged to Abaqus's propagation: zero-valued
boundary conditions active in every step go to the initial state, and steps restate their
boundary conditions and loads with `OP=NEW` when the active set changes.
- Nastran (`modelcraft_decks::nastran`): entries with a real use large (16-column) fields, the rest
small fields; a real is exact when its shortest round-trip form fits 16 columns, else rounded to
at least ten significant digits. Linear solids map full integration to `PSOLID` `TWO`/`THREE` +
`FULL`, hex20 reduced to `TWO` + `FULL`, hex8 incompatible modes to `BUBBLE`; one-point reduced
linear solids, hybrid solids, reduced-integration or one-point shells, body forces, gravity on part
of the model, orthotropic beams and rods, and orthotropic shells off planes of constant Z are
reported as unsupported. Static and frequency steps need separate decks (`deck.write` `steps`).
- LS-DYNA (`modelcraft_decks::lsdyna`, `deck.write {"format": "lsdyna"}`): long format (20-column
fields; every value with up to 13 significant digits, and 17-digit values from 0.01 to 1e17, are
written exactly; the rest is rounded to at least 13 digits and counted). The 10-node tetrahedron
follows the manual's figure: mid-side nodes 8, 9, 10 on edges 2-4, 3-4, 1-4 (the model has them
on 1-4, 2-4, 3-4). Incompatible modes map to ELFORM −18 (eight-point enhanced strain). Several
steps are written as `*CASE` analyses. Refused with the item named: beam sections (not yet),
body forces per volume, partial-DOF kinematic couplings, constraints on a coupled reference
point, gravity on different sets or on parts of sections, hybrid other than tet4, reduced
quadratic elements, materials without density, more than 10 shell integration points.
- Open item (LS-DYNA tet10 node order): the writer follows the manual's figure (mid-side nodes 8,
9, 10 on edges 2-4, 3-4, 1-4), which disagrees with an earlier reading as the Abaqus order. It
needs one confirmation run by a licensed user; agents never run commercial solvers.