forked from 1b-agent/fieldcraft-upstream
* Model, fem and decks: point masses, rotary inertia, springs, dashpots and rod3 trusses Model: PointMass and Spring definitions (spring | dashpot; to ground or two-point; along a degree of freedom, a vector or the line of the ends) on a set or reference point, resolved per node; ElementKind::Rod3. fem: rod2/rod3 truss kernel on Basis::Line2/Line3 declaring ElementDofs (translations). Decks: Abaqus T3D3, MASS, ROTARYI, SPRING1/2/A, DASHPOT1/2/A; Nastran CONM1, CELAS2, CDAMP2; LS-DYNA ELEMENT_MASS/INERTIA and ELEMENT_DISCRETE; what a format cannot take is reported. Commands model.mass.* and model.spring.*. Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com> Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm * Implicit solver: trusses, point masses, rotary inertia and springs on the DofLayout Trusses declare their translations like solids; point masses, inertia and springs ask the layout for the kinds they need at their nodes (translations, rotations), and reference points they use get six degrees of freedom. The matrix pattern takes rows for those points; dashpots are ignored with a warning. Existing results are bit-identical (hash-checked). Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com> Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm * Explicit solver: trusses, point masses, springs and dashpots on the node-major layout Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com> Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm * docs: fem.md on trusses and discrete elements in the layout; regenerate features.md Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com> Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm * docs: trusses in plane models and corotational explicit trusses 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>
89 lines
5.8 KiB
Markdown
89 lines
5.8 KiB
Markdown
# Element library
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ModelCraft's finite element library (`crates/fem`), family by family, with status. The scope is
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modelled on what a full CAE code offers (Abaqus's element library is the reference for breadth);
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names, formulations and tests are our own, written from the published literature. Deck writers map
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each of our elements to each solver's name (see `crates/decks`). Simple elements first: 1D and 2D,
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then shells, special-purpose and multiphysics elements.
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Status: **done** (on main, verified against analytic solutions), **in progress** (an agent task is
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open), **planned**.
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Every element builds on the shared foundation of docs/fem.md: it declares its nodal degrees of
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freedom (`DofKind`: translations, rotations, temperature, pressure) and condensed internal ones
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(`ElementDofs`), the solvers number them with `DofLayout`, and its interpolation comes from the
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shape-function library (`Basis`: line2/3, tri3/6, quad4/8/9, tet4/10, wedge6/15, pyramid5,
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hex8/20/27 with first and second derivatives).
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## Point and discrete elements
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| Element | Use | Status |
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| Point mass | Lumped mass at a node or reference point (isotropic or per direction) | done (implicit, explicit; Abaqus MASS, Nastran CONM1, LS-DYNA ELEMENT_MASS; per direction: Nastran only) |
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| Rotary inertia | Inertia tensor at a 6-DOF node | done (implicit; Abaqus ROTARYI, Nastran CONM1, LS-DYNA ELEMENT_INERTIA; explicit when it has rotations) |
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| Spring to ground / two-point spring | Linear spring in a fixed direction or along the line of nodes | done (implicit, explicit translational; Abaqus SPRING1/2/A, Nastran CELAS2, LS-DYNA ELEMENT_DISCRETE; skew fixed directions: LS-DYNA only) |
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| Dashpot to ground / two-point | Linear viscous damper (dynamic steps; ignored in static) | done (explicit; ignored with a warning in static and frequency steps; Abaqus DASHPOT1/2/A, Nastran CDAMP2, LS-DYNA ELEMENT_DISCRETE) |
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| Nonstructural mass | Mass spread over a region without stiffness | planned |
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| Connectors | Kinematic joints (hinge, slot, universal…) with elasticity, damping, stops | planned (M7) |
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## 1D elements
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| Element | Use | Status |
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| Truss, 2-node (2D and 3D) | Axial members, cables (compression allowed) | done (rod2: implicit, in plane models with their two unknowns per node; explicit, corotational under nonlinear geometry; Abaqus T3D2 / T2D2, Nastran CROD, LS-DYNA truss beam (3D models)) |
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| Truss, 3-node (2D and 3D) | Curved axial members | done (rod3: implicit, plane models too; explicit with small displacements; Abaqus T3D3 / T2D3; no Nastran or LS-DYNA counterpart) |
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| Beam, 2-node Timoshenko, 3D | Frames, stiffeners; shear deformable | in progress (shells and beams) |
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| Beam, 2-node Euler–Bernoulli (cubic), 2D and 3D | Slender frames; exact for end-loaded prismatic members | planned (1D elements II) |
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| Beam, 3-node Timoshenko (quadratic), 2D and 3D | Curved and stocky beams | planned (1D elements II) |
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| Beam, 2D (planar frames) | In-plane frames with 3 DOFs per node | planned (1D elements II) |
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| Pipe / elbow | Pipes with internal pressure, ovalisation | planned (1D elements II) |
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| Open-section beams with warping | Thin-walled sections in torsion | planned |
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| Rebar / stringers | Reinforcement along edges or embedded | planned |
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## 2D elements
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| Element | Use | Status |
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| Plane stress tri3, tri6, quad4, quad8 | Thin plates loaded in their plane | in progress (2D elements) |
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| Plane strain tri3, tri6, quad4, quad8 | Long sections (dams, tunnels, extrusions) | in progress (2D elements) |
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| Axisymmetric tri3, tri6, quad4, quad8 | Revolved solids (shafts, vessels, discs) | in progress (2D elements) |
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| Incompatible-mode and reduced-integration quads | Bending-accurate and cheap variants | in progress (2D elements) |
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| Generalized plane strain | Plane strain with a free out-of-plane strain | planned |
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| Axisymmetric with twist | Revolved parts under torsion | planned |
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| Axisymmetric shells (2-node, 3-node) | Thin revolved shells (tanks, domes) | planned |
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| Hybrid (mixed u–p) variants | Nearly incompressible materials | planned |
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## Shells and membranes
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| Element | Use | Status |
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| Shell quad4 (MITC4), triangle (locking-free) | Thin and thick shells | in progress (shells and beams) |
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| Shell quad8 / tri6 | Curved thick shells | planned |
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| Continuum shells (8-node, on swept hex) | Thick-to-thin shells, composites through thickness | planned (M8) |
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| Membranes (tri3, quad4, quad8) | Fabrics, inflatables, skins without bending | planned |
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| Surface elements | Massless surfaces for loads and contact | planned |
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| Composite layups on shells | Ply tables, orientations | planned (M8) |
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## 3D solids
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| Element | Use | Status |
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| tet4, tet10 | Free meshes of any part | done |
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| hex8 (full, incompatible modes), hex20 (full, reduced) | Structured and swept meshes | done |
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| wedge6 | Swept meshes from triangles, transitions | done |
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| hex8 one-point with hourglass control, nodal-pressure tet4 (explicit) | Explicit dynamics | done |
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| wedge15, pyramid5/13 | Quadratic transitions, tet–hex transition | planned (M5); wedge15 and pyramid5 shape functions done |
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| Hybrid (mixed u–p) solids | Nearly incompressible materials (rubber) | in progress (FEM foundation, phase C); pressure DOF kind done |
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| Modified quadratic tet (tet10 for contact/plasticity) | Robust quadratic tets | planned |
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## Special-purpose and multiphysics
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| Element | Use | Status |
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| Cohesive (2D, 3D) | Adhesive layers, delamination | planned |
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| Gasket | Through-thickness gasket behaviour | planned |
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| Infinite elements | Unbounded domains | planned |
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| Heat transfer (all shapes), coupled temperature–displacement | Thermal and thermal-stress analyses | in progress (FEM foundation, phase B); temperature DOF kind done |
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| Acoustic | Fluid acoustics, structural–acoustic coupling | planned |
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| Rigid elements | Rigid bodies from meshes | planned (M7) |
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