OneCAD-Simulation/docs/fem.md

FEM foundation: degrees of freedom and shape functions

What every element in crates/fem and every solver builds on. Code: crates/fem/src/dof.rs, crates/fem/src/basis.rs, crates/fem/src/jet.rs.

Degrees of freedom

Every unknown is a pair (node, DofKind):

DofKind	Meaning	Model / deck number
Ux, Uy, Uz	translations along X, Y, Z	1, 2, 3
Rx, Ry, Rz	rotations about X, Y, Z	4, 5, 6
P	pressure (mixed u–p elements)	8
T	temperature	11

The enum order (Ux, Uy, Uz, Rx, Ry, Rz, T, P) is the numbering order within a node. DofKind::from_number / number convert to the 1-based numbers boundary conditions use; from_direction / direction to the structural directions 0–5.

Elements declare their unknowns with ElementDofs { node: DofSet, internal: Internal }: the kinds every node of the element carries (DofSet::TRANSLATIONS for solids, PLANE for 2D elements, STRUCTURAL for shells and beams, TEMPERATURE for heat transfer, translations plus PRESSURE for continuous-pressure mixed elements) and the internal unknowns the element condenses out itself (incompatible_modes, discontinuous pressure), which never reach the global system. An element's matrices are ordered node by node, its node kinds in DofKind order within a node (a shell's 24 × 24 stiffness: node 1 Ux Uy Uz Rx Ry Rz, node 2 …). Solid elements: Formulation::dofs() / Solid::dofs().

Numbering (DofLayout): collect what every node needs with DofLayout::builder() (element(labels, dofs), node(label, kinds) for constraints and boundary conditions that need a kind no element gives, point(label, kinds) for reference points), then build(). A node carries the union of what was asked for. Unknowns are numbered mesh nodes in label order, each node's kinds in DofKind order, then the points in the order added; a slot's unknowns are contiguous, so a node pair is one dense block in the assembled matrix. The same model always gives the same numbering.

Lookups: node(label) / slot(label) (a slot is a position: mesh nodes 0..nodes(), points point_slot(k)), dof(slot, kind), range(slot), kinds(slot), locate(dof) -> (slot, kind), element_dofs(slots, kinds), describe(dof), stride() (uniform layouts).

Trusses declare fieldcraft_fem::truss::DOFS (translations, on Basis::Line2/Line3). Point masses, springs and dashpots are not mesh elements: the implicit solver asks the layout for what each needs at its nodes (fieldcraft_solver::discrete::needs: translations for a mass or a translational spring, rotations for an inertia or a torsional spring; a reference point they use is a point with six) and finds its unknowns with discrete::dof_of.

Solvers: fieldcraft_solver::system::Mesh::layout numbers the implicit system (mesh nodes, then six per coupled reference point); assembly (sparse::add_block(k, layout, slots, kinds, data), add_scalar, add_diagonal) works for any mix of kinds per node, so a solid sharing nodes with a shell adds its translation block into the shell nodes' six-unknown blocks. Boundary conditions and loads address (node, kind): a boundary condition holds the kinds a node carries, and a moment needs rotations. The explicit solver has solid nodes only and checks that its layout is the uniform node-major one (NODE_DOFS = 3).

Shape functions

Basis is every family's interpolation:

Family	Reference element	Nodes
Line2, Line3	ξ ∈ [−1, 1]	ends −1, 1; line3 adds the middle
Tri3, Tri6	ξ, η ≥ 0, ξ + η ≤ 1	corners (0,0), (1,0), (0,1); mid-sides of 1-2, 2-3, 3-1
Quad4, Quad8, Quad9	[−1, 1]²	corners counter-clockwise from (−1,−1); mid-sides of 1-2, 2-3, 3-4, 4-1; centre
Tet4, Tet10	unit tetrahedron	corners (0,0,0), (1,0,0), (0,1,0), (0,0,1); mid-sides of 1-2, 2-3, 3-1, 1-4, 2-4, 3-4
Wedge6, Wedge15	triangle × ζ ∈ [−1, 1]	bottom 1-3, top 4-6; mid-sides of the bottom edges, top edges, vertical edges
Pyramid5	base [−1, 1]² at ζ = 0, apex (0, 0, 1)	base corners as quad4, then the apex
Hex8, Hex20, Hex27	[−1, 1]³	corners 1-4 at ζ = −1, 5-8 above; hex20 mid-sides (bottom, top, vertical edges); hex27 face centres in ElementKind::Hex8.faces() order, then the centre

Node orders are the model's (ElementKind::edges() / faces() are the single source): corners, mid-side nodes in edge order, face nodes, body nodes. Basis::of(ElementKind) maps a model element; nodes() gives natural node coordinates; dim(), count(), corners(), degree() (the complete polynomial degree reproduced: 1 for linear families including the rational pyramid, 2 for the quadratic ones).

Evaluation at a natural point xi: [f64; 3] (unused coordinates are zero):

• eval(xi) -> Shape: values n and first derivatives dn[i] = ∂Nᵢ/∂(ξ, η, ζ). tet4, tet10, wedge6, hex8, hex20 use the hand-written functions of shape.rs (the solid kernels' path).
• eval2(xi) -> Shape2: adds d2n[i][a][b] = ∂²Nᵢ/∂ξₐ∂ξ_b, from second-order forward-mode automatic differentiation of the same formulas (jet::Jet): exact to round-off.
• gradients(&shape, xyz) -> Gradients: physical dx[i] = ∇ₓNᵢ = J⁻¹ ∇_ξNᵢ and det J, with J_ab = ∂x_b/∂ξₐ; an inverted or collapsed element is Error::Degenerate.
• hessians(&shape2, xyz) -> Hessians: physical d2x[i] = J⁻¹ (H_ξ − Σ_b (∂N/∂x_b) X_b″) J⁻ᵀ with X_b″ = Σᵢ x_{i,b} H_ξ(Nᵢ), the map's second derivative (T. J. R. Hughes, The Finite Element Method, 2000, §3.9, §4.2), and laplacian(i). Without the X″ term a field linear in x would have a nonzero Hessian on a curved element.

A family of dimension d maps onto the first d physical coordinates (plane elements in x–y, lines along x). Elements embedded in a higher dimension (shells, beams, trusses in 3D) pass node coordinates in their own local frame.

Verification (basis::tests, dof::tests, jet::tests)

For every family: Kronecker delta at the nodes; partition of unity (Σ N = 1, Σ ∇N = 0, Σ H = 0); exact reproduction of every monomial up to degree() with its gradient and Hessian in natural coordinates; first and second derivatives against central differences; on an affine map, physical gradients, Hessians and Laplacians exact for a complete polynomial of the family's degree; on a curved map, linear fields exact with zero Hessian, and the physical Hessian of a quadratic interpolant consistent with finite differences of its physical gradient. The solver and explicit migration to DofLayout was checked bit for bit: every result of the solver, explicit, engine and io test suites hashes identically before and after.

Heat transfer and thermal strain

A heat conduction element carries one temperature per node (heat::HEAT_DOFS, kind T); heat::Conduction gives the conductivity ∫ ∇Nᵀ k ∇N dV (full rule), the capacity ∫ ρc N Nᵀ dV and a source ∫ N Q dV (mass rule), and the heat flux −k∇T at the integration points; heat::face_weights and face_film integrate surface flux and convection on tri3/tri6/quad4/quad8 faces. The solver (fieldcraft_solver::heat) numbers the temperatures with DofLayout::uniform(…, DofSet::TEMPERATURE) and assembles with the same sparse::add_block.

Thermal strain ε_th = α (T − T_ref) along the material axes enters a solid as the load Solid::thermal_load(d, &ThermalStrain { alpha, delta }) = ∫ Bᵀ D ε_th dV and its stress as Solid::stresses_with(d, u, Some(&thermal)) = D (ε − ε_th); delta is the nodal T − T_ref. 2D elements have the same pair (Plane::thermal_load, Plane::stresses_with): plane stress leaves εzz free (σzz = 0), plane strain holds it (σzz = −D₃·ε_th), axisymmetric elements strain the hoop direction too. Trusses (rod2, rod3) take the axial part Σ αₖ tₖ² ΔT along their tangent (Truss::thermal_load, Truss::stresses_with). Shells and beams will provide the same two functions for their strains; springs, dashpots and point masses have no thermal strain.

Explicit dynamics takes a step's temperature loads as a thermal strain rate per element, α ΔT / end time (the change reached linearly over the step, like a prescribed displacement, so there is no thermal shock), subtracted from each increment's strain increment before the constitutive update, so it feeds J2 and Johnson–Cook plasticity alike; isotropic expansion only (the rate is the same in any frame). Explicit trusses take no thermal strain yet (a warning says so).

Model side: Material::thermal (conductivity, specific_heat, expansion, each isotropic or per axis, and reference_temperature), BoundaryCondition::Temperature, loads SurfaceFlux, Convection, HeatSource (heat transfer) and Temperature (a temperature field in a static step), procedures HeatTransfer { transient } and CoupledTemperatureDisplacement. Commands: solve.heat, and solve.static for coupled steps. The deck writers refuse heat transfer by name for now.

Hybrid (mixed u–p) solids

A section with "formulation": {"hybrid": true} gives Formulation::Hybrid { pressures } (crate::hybrid): the isotropic elasticity splits as D = D_dev + K m mᵀ, the mean stress is an independent field discontinuous between elements (hex20: 1, x, y, z; hex8 and tet10: constant), and it is condensed out element by element, p̂ = K M⁻¹ Gᵀ u, leaving the stiffness K_dev + K G M⁻¹ Gᵀ. ElementDofs.internal.pressure counts the condensed unknowns; nothing global changes, and Cholesky still applies. Stresses are D_dev ε + p m with the element's pressure field. The choice of pressure space follows the inf-sup analysis (docs in crates/fem/src/hybrid.rs): Q2–P1disc and P2–P0 are stable; Q1–P0 does not lock but may show checkerboard pressures; linear tetrahedra and wedges lock even so and are refused. A thermal strain splits the same way: ∫ Bᵀ D_dev ε_th on the nodes and, through the pressure, K G M⁻¹ ∫ N_p tr ε_th, so a heated nearly incompressible solid takes its bulk stress −3KαΔT when confined. A continuous nodal pressure (DofKind::P, Taylor–Hood) needs a symmetric indefinite factorization and is planned.

Symmetric indefinite factorization (LDLᵀ)

fieldcraft_solver::ldlt factors P A Pᵀ = L D Lᵀ (L unit lower triangular, D with 1 × 1 and 2 × 2 pivots) on the Cholesky factor's symbolic factorization: the same nested dissection ordering, elimination tree, supernodes, fill, factor-size cap and parallel subtree tasks, so it is deterministic on any number of threads. Pivots are chosen by the bounded Bunch–Kaufman (rook) search of Ashcraft, Grimes & Lewis (1998) among the columns of the supernode being factored (Schenk & Gärtner's supernode Bunch–Kaufman, 2006): an interchange inside a supernode changes no row structure, so nothing is delayed and the static structure holds. Its limits, stated in the module: L's entries below the supernode are not bounded by the search (solve_refined adds iterative refinement), and a column whose supernode offers no pivot above round-off is a located Singular error (a matrix singular at that column, or a zero diagonal coupled only to later supernodes, which no FieldCraft system has: hybrid pressures are condensed per element).

The factor reports its inertia (positive and negative eigenvalue counts, Sylvester's law): a 2 × 2 pivot of the search has a negative determinant (one of each). Symmetric::new(a, cap, kind) picks Cholesky (Definite, the default everywhere a matrix is positive definite, so linear results are bit for bit unchanged), LDLᵀ (Indefinite), or Cholesky with LDLᵀ when the matrix turns out not to be positive definite (Auto, one symbolic factorization for both). On a hex8 stiffness pattern of 140 000 equations (1.5 · 10⁸ entries) the LDLᵀ factor costs 1.1 times the Cholesky factor, and 1.2 times on a shift with 10 600 negative eigenvalues and 7 700 2 × 2 pivots (ldlt::tests::speed_against_cholesky).

Nonlinear static analysis (finite strain)

A step {"type": "nonlinear_static", …} (Procedure::NonlinearStatic, solved by solve.nonlinear, fieldcraft_solver::nonlinear) follows equilibrium in load increments with Newton–Raphson iterations. The step's load factor λ runs from 0 to 1: dead loads are λ times their values, a pressure follows the deformed faces with λ times its magnitude, and prescribed displacements are λ times theirs (a linear ramp).

Material point (fieldcraft_fem::constitutive). Given the deformation gradient F and the history committed at the end of the last converged increment, a material returns the Kirchhoff stress τ = J σ and the spatial tangent c of its Lie derivative (L_v τ = c : d), in Voigt order with engineering-shear columns, so c = D at F = I. This is the push-forward of the second Piola–Kirchhoff stress and its tangent: τ = F S Fᵀ, c_ijkl = F_iI F_jJ F_kK F_lL C_IJKL. History variables (MaterialModel::history_len per integration point) are read from the committed slice and written to a separate one, which the solver commits when the increment converges, so a cut-back increment leaves no trace. The materials:

Material in a nonlinear step	Model
Elastic (isotropic or orthotropic), no option	St Venant–Kirchhoff: S = D E, E = ½(FᵀF − I). Right for large rotations with small strains; it softens without bound in large compression.
Isotropic elastic with "hyperelastic": {"type": "neo_hookean"}	Compressible neo-Hookean with the isochoric–volumetric split, W = μ/2 (Ī₁ − 3) + κ/2 (J − 1)², μ and κ from E and ν (C₁₀ = μ/2, D₁ = 2/κ). Its small-strain limit is the linear material, which linear steps use.
Isotropic elastic with {"type": "mooney_rivlin", "c01": …} or {"type": "yeoh", "c20": …, "c30": …}	Decoupled polynomials W̄ = C₁₀ (Ī₁ − 3) + C₀₁ (Ī₂ − 3) + C₂₀ (Ī₁ − 3)² + C₃₀ (Ī₁ − 3)³ with the same volume κ/2 (J − 1)²: Mooney–Rivlin with C₁₀ = μ/2 − C₀₁ (0 ≤ C₀₁ ≤ μ/2), Yeoh with C₁₀ = μ/2, so 2(C₁₀ + C₀₁) is the elastic μ and the small-strain material stays the elastic one. Stress and tangent from the fictitious τ̄ and c̄ (Holzapfel 2000, eqs. 6.168, 6.193). Abaqus *HYPERELASTIC, MOONEY-RIVLIN / YEOH; LS-DYNA refuses them by name.

| Isotropic elastic with "plastic" (bilinear isotropic or kinematic, table, Johnson–Cook) | J2 plasticity (fieldcraft_fem::elastoplastic): at finite strain Simo's multiplicative model (CMAME 99, 1992) with a Hencky elastic energy, τ = K ln J I + 2G dev ½ ln bₑ, the history Cₚ⁻¹ and the equivalent plastic strain, integrated by the exponential return map on the principal logarithmic strains; at small strain the additive radial return with the back stress. Both call J2::radial_return, the update of explicit dynamics, and its consistent tangent J2::tangent. |

Plasticity's tangent. With Cₚ⁻¹ frozen over an iteration, L_v τ = 𝔻ᵉᵖ : ½ (∂ ln b/∂b) : (d b + b d) − (d τ + τ d), 𝔻ᵉᵖ the algorithmic tangent of the return (K I⊗I + 2Gθ ℙ − 2Gθ̄ n⊗n, Simo & Hughes 1998 Box 3.2) and the derivative of the logarithm the Daleckii–Krein divided differences θ_AB = artanh(r)/r, r = (λ²_A − λ²_B)/(λ²_A + λ²_B), in the principal frame of the trial bₑ: smooth through equal stretches, so uniaxial and undeformed states need no special case. The tangent is symmetric (isotropic hardening) and checked against central differences of the stress and of every element's forces from a plastic history. Hybrid elements take the deviatoric return and the volume K/2 (ln J)². Refused by name in nonlinear steps: kinematic hardening at finite strain (a back stress is not coaxial with bₑ, which the principal-frame return needs; it works with small strain), the Johnson–Cook strain-rate term (a static step has no time; C = 0 is the rate-independent law), and incompatible-mode elements of a plastic material. Damage, erosion and adiabatic heating act in explicit dynamics only (a warning says so). A hardening slope below −3G leaves the point without a tangent: the increment cuts back and the step stops at the minimum increment, naming the element.

"Isotropic elastic" keeps meaning the same thing everywhere: the neo-Hookean model is chosen only by the explicit option, and explicit dynamics refuses a hyperelastic material by name.

Elements (fieldcraft_fem::finite), total Lagrangian over the reference element with its own quadrature: f_a = ∫ Bₓ,aᵀ τ dV₀ and K_ab = ∫ (Bₓ,aᵀ c Bₓ,b + ∇ₓN_a·τ∇ₓN_b I) dV₀ with the current gradients ∇ₓN = F⁻ᵀ∇₀N (material plus geometric stiffness), identical term by term to ∫ B₀ᵀ S dV₀ and its linearisation. Every element's tangent is checked against central differences of its forces.

Element	Nonlinear steps
tet4, tet10, wedge6, hex8, hex20 (full), hex20 (reduced)	total Lagrangian
hybrid hex8, hex20, tet10	Simo–Taylor–Pister three-field form on the linear hybrid elements' pressure fields (θ the projection of J, p the projection of U′(θ)); needs the neo-Hookean option (St Venant–Kirchhoff has no volumetric split)
hex8 and quad4 incompatible modes	refused: their finite-strain form (enhanced assumed strain, Simo–Armero 1992) needs the modes as unknowns carried between iterations and hourglasses in large compression; use full integration, hybrid or quadratic elements
plane strain, axisymmetric (tri3, tri6, quad4, quad8)	total Lagrangian with F₃₃ = 1 or r/R (hoop column N/r, geometric term τ_θθ N_a N_b/r²)
plane stress	refused (σ_zz = 0 needs a local iteration for the thickness)
trusses, shells, beams	refused (large rotations of structural elements come later in M15)

Without nonlinear geometry ("nonlinear_geometry": false) an elastic element is the linear one (K u), and an element of a plastic material takes the same loops with small strain (Kinematics::Small: ε = sym ∇u, the reference gradients, f = ∫ Bᵀσ dV, K = ∫ Bᵀ𝔻B dV with the consistent tangent, no geometric stiffness; hybrid elements project 1 + tr ε and K tr ε), so an elastic model is still the linear solution reached by Newton.

Follower pressure (fieldcraft_fem::face::follower_pressure, follower_edge_pressure): fᵢ = −p ∫ Nᵢ (x,ξ × x,η) dξ dη on the current face, with its load stiffness K = p ∫ N_a (N_b,η [x,ξ]× − N_b,ξ [x,η]×). The load stiffness is not symmetric. The solver keeps its symmetric part and leaves the skew part out, so the tangent stays symmetric for the supernodal Cholesky factorization: the residual is exact (the converged answer does not change), and over a closed surface or one whose boundary is held the skew parts of neighbouring faces cancel (Schweizerhof & Ramm 1984), so nothing is lost there; elsewhere Newton may converge linearly instead of quadratically, and the result says how large the left-out part is. An LU factorization would double the factor's memory and lose the symmetric solver for a gain only in the rate of convergence of open loaded surfaces; it is revisited with the symmetric indefinite (LDLᵀ) factorization that arc-length and Taylor–Hood need. Without nonlinear geometry a pressure is a dead load.

Load path. A step's load_path, [[fraction, factor], …] from [0, 0] to fraction 1, makes the load factor piecewise linear in the step fraction (without one it equals the fraction), so loads and prescribed displacements can come down or reverse within a step: cyclic loading. Increments end at every point of the path, and the extrapolated predictor scales with the change of the load factor, so it turns with the path. LS-DYNA writes the path as the step's curve; Abaqus refuses it by name for now (it would be an amplitude on every load and boundary condition).

Predictors. An increment starts from the linear extrapolation of the last one; with path-dependent materials an increment without one (the first, after a turn of the path to zero change) starts from the tangent predictor: one solve with the converged state's tangent for the change of the loads and of the prescribed displacements, so a prescribed motion is spread into the interior before the material sees it (started from the boundary's jump alone, the elements next to it would flow plastically far beyond the solution). Its work is then the energy criterion's reference. A first tangent that is not positive definite is a cutback when the undeformed model's tangent is (the strain of the increment, not a model that can move freely).

Newton–Raphson with the consistent tangent refactored every iteration, an optional line search (off by default: on large elastic rotations the full step converges in fewer iterations), and convergence when the force residual (∞-norm over the largest force seen), the displacement correction (over the increment's largest displacement) and the energy (over the first iteration's) are all below their tolerances, or the residual is round-off. Each increment starts from the linear extrapolation of the last one. Automatic incrementation grows an increment by half after two fast ones (≤ 4 iterations), shrinks it after a slow one (> 8), and cuts it to a quarter when an element inverts, the residual is not finite or grows twice, the tangent is singular, or the iterations run out; the step stops with the load factor and the reason at the minimum increment, the increment cap, or Limits::max_newton_iterations.

Indefinite tangents. A tangent that is not positive definite (a strained nearly incompressible mixed element, an unstable material, a state past a limit or bifurcation point) is factored by LDLᵀ and Newton goes on; each iteration records the tangent's negative eigenvalues, and the summary warns when a converged state keeps some (an unstable equilibrium under load control). This lifts the old limit on hybrid elements near ν = ½ under prescribed displacement (at ν = 0.4999 every increment used to be cut back to the cap). Only the first tangent of a model that can move freely is an error. The tangent predictor of path-dependent materials keeps Cholesky and is skipped when the tangent is indefinite.

Results: the final displacements and reactions, the Cauchy stress and the logarithmic strain (ln V, engineering shears; the small strain without nonlinear geometry) at the integration points and averaged at the nodes, the equivalent plastic strain at the integration points of plastic elements (solve.probe with elements, the largest in the step summary), every increment's load factor, iterations and residuals, and a displacement frame per converged increment (results.frame, the slider in the results panel).

Couplings stay the linear constraints of the linear solver (small rotations of the reference points), with a warning; springs act along their fixed directions. Centrifugal loads are refused by name in nonlinear steps.

Thermal strain. A nonlinear step's temperatures are its temperature loads, or the steady conduction of its temperature boundary conditions and heat loads solved first (one-way, as the linear coupled temperature–displacement step); they ramp with the load factor from each material's reference temperature. With nonlinear geometry F = F_m F_θ, F_θ = diag(1 + αᵢ ΔT) at each integration point (V. A. Lubarda, Appl. Mech. Rev. 57:95–108, 2004): the material sees F_m, the loops run on the expanded volume J_θ dV₀ (mixed elements project det F_m), and the reported strain is the total logarithmic one; the linear stretch 1 + α ΔT keeps α the engineering coefficient, so a free body grows by exactly α ΔT. Without nonlinear geometry the split is additive (ε_m = ε − α ΔT), and elastic elements on their linear stiffness take the equivalent nodal forces as a dead load. Johnson–Cook plasticity softens at the point's temperature. The expansion is constant in temperature (the model has no temperature-dependent coefficient yet).

Decks: Abaqus *STEP, NLGEOM=YES|NO, INC= with *STATIC (initial, period 1, minimum, maximum) and *CONTROLS, PARAMETERS=LINE SEARCH; the neo-Hookean option as *HYPERELASTIC, NEO HOOKE; plasticity as for explicit dynamics (*PLASTIC); a load path, and a plastic deck of several general steps (Abaqus carries the plastic state from one to the next, every model step starts undeformed), are refused. LS-DYNA: the ramped implicit run with full Newton (ilimit 1, maxref) and *CONTROL_IMPLICIT_AUTO; hyperelastic materials in nonlinear steps and steps without nonlinear geometry are refused; a load path is the step's curve. Nastran refuses nonlinear steps (SOL 400) by name. Iteration caps and tolerances are left to each solver's own controls, whose norms differ from ours.

Verification (crates/solver/tests/nonlinear.rs, crates/fem/src/{constitutive,finite,face}.rs, and tests/oracle/nl-*): consistent tangents of both materials and of every element (central differences); uniaxial stretch to λ = 2 of a neo-Hookean block in every element kind, plane strain and axisymmetric (closed form); St Venant–Kirchhoff uniaxial stretch; the nonlinear patch test on a distorted mesh (all solids, hybrid ones included); a 90° rigid rotation (zero stress); the elastica (Bisshopp–Drucker) at P L²/(E I) = 1, 2, 5, 10 with hex20 (0.2–0.5 %); the inflation of a thick neo-Hookean tube by a follower pressure (Rivlin's closed form); Newton's quadratic convergence; the linear limit; a finite-strain Cook's membrane is pending its transcribed reference; and the failures (an element inverted by crushing stops at the minimum increment, naming it; the caps; what is refused). Plasticity (crates/solver/tests/plasticity.rs, crates/fem/src/elastoplastic.rs, tests/oracle/ nl-j2-uniaxial, j2-bauschinger, plastic-thick-cylinder, plastic-hinge-cantilever): the consistent tangents against central differences from a plastic history (material point and every element, finite and small strain, full and hybrid); uniaxial tension to a logarithmic strain of 0.2 in every element kind, hybrid ones included (Kirchhoff stress exact to 10⁻⁷, and 0.13 % from explicit dynamics' hypoelastic Cauchy stress, the elastic volume change between the two laws); the Bauschinger effect on a load path back to zero strain (exact); Hill's thick cylinder, the bore displacement at a plastic radius of 1.5a (0.009 %) and the collapse pressure (2·10⁻⁸); a cantilever's collapse 3.1 % above beam theory's hinge, converged under refinement; Newton's order with the consistent tangent 1.9 (small strain) and 2.3 (finite strain) in a plastic cantilever; and the refusals and the softening material that stops at the minimum increment. Mooney–Rivlin and Yeoh (nl-mooney-rivlin-modes, nl-yeoh-uniaxial, nl-mooney-rivlin-tube): tangents by central differences (material point and hybrid elements), Treloar's uniaxial, equibiaxial and pure-shear modes against the compressible closed form (exact), and a tube inflated by a follower pressure while stretched axially to λ_z = 1.5 (Rivlin's incompressible solution, 0.6 % at ν = 0.4995). Thermal strain (nl-thermal-expansion, j2-heated-bar, crates/solver/tests/nonlinear_thermal.rs): free expansion and a fully held block at a thermal stretch of 1.2 (exact, full and hybrid), a bar held at its ends heated past yield (exact), the linear limit against the linear and coupled solvers, and tangents with a temperature field.