forked from 1b-agent/fieldcraft-upstream
FEM foundation B: heat transfer and thermal stress (solids, 2D, explicit), coupled temperature–displacement, solve.heat (#45)
* Heat transfer and thermal stress: thermal materials, temperature BCs, heat loads, heat transfer and coupled temperature–displacement steps, solve.heat
Model: Material.thermal (conductivity, specific heat, expansion, isotropic or
per axis; reference temperature), BoundaryCondition::Temperature (dof 11),
loads SurfaceFlux, Convection, HeatSource and Temperature (a field in static
steps), procedures HeatTransfer { transient (θ-method) } and
CoupledTemperatureDisplacement; checks for missing conductivity/specific
heat/expansion. fem: heat conduction kernels (conductivity, capacity,
source, face flux/film, heat flux) on the DofLayout (one T per node), thermal
strain load and stress D(ε − ε_th) for every solid formulation incl.
incompatible modes. Solver: steady and transient heat transfer, thermal loads
in static steps, coupled steps (exact one-way coupling). Engine: solve.heat,
temperature/heat-flux result fields, probes. Decks refuse heat transfer by
name. Analytic verification: slab, source+convection/flux, thick cylinder,
erfc semi-infinite solid, free/constrained expansion, bimetal strip, coupled
step.
Co-Authored-By: Claude Opus 5.5 <[email protected]>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm
* thermal: strains in 2D elements and explicit dynamics
Plane::thermal_load and stresses_with for plane stress (εzz free), plane
strain (σzz = −D₃·ε_th) and axisymmetric elements, incompatible modes
included; the solver's 2D kernels take them. Explicit dynamics turns a
step's temperature loads into a per-element thermal strain rate (reached
linearly over the step) subtracted from each strain increment, so it feeds
J2 and Johnson–Cook updates. Verified: free expansion in every 2D theory
and element, a biaxially held plate, an explicit free bar (ΔL = αΔT L,
stress-free) and a clamped bar at −EαΔT, capped at the yield stress with
perfect plasticity.
Co-Authored-By: Claude Opus 5.5 <[email protected]>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm
* clippy
Co-Authored-By: Claude Opus 5.5 <[email protected]>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm
* thermal: trusses take the axial thermal strain; keep the roadmap's M7 line
Truss::thermal_load and stresses_with project the thermal strain on the
member's tangent (Σ αₖ tₖ² ΔT); the static solver applies them to rod2/rod3
(#38). Explicit trusses take none yet and a warning says so.
Co-Authored-By: Claude Opus 5.5 <[email protected]>
Claude-Session: https://claude.ai/code/session_01NmAttHhUZTokgPeEJia8sm
---------
Co-authored-by: jyviko <[email protected]>
Co-authored-by: Claude Opus 5.5 <[email protected]>
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@@ -327,6 +327,7 @@ impl<'m> Deck<'m> {
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self.plan_discrete()?;
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self.plan_constraints()?;
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self.plan_loads()?;
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self.problems.extend(crate::thermal_items(self.model));
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for sub in &mut self.subcases {
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if matches!(sub.step.procedure, Procedure::Frequency { .. }) {
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sub.method = Some(next_id(&mut self.next_sid)?);
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@@ -705,6 +706,8 @@ impl<'m> Deck<'m> {
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OutputVariable::ReactionForce => "SPCFORCES",
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OutputVariable::Stress => "STRESS",
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OutputVariable::Strain => "STRAIN",
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// Heat transfer steps are refused (thermal_items).
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OutputVariable::Temperature | OutputVariable::HeatFlux => continue,
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};
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let _ = writeln!(out, " {request} = ALL");
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}
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@@ -928,7 +931,7 @@ impl<'m> Deck<'m> {
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let a = angular_velocity / (2.0 * std::f64::consts::PI);
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entry(Card::new("RFORCE").int(*sid).blank().blank().real(a).reals(*axis), out, &mut first)?
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}
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Load::BodyForce { .. } => {}
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Load::BodyForce { .. } | Load::SurfaceFlux { .. } | Load::Convection { .. } | Load::HeatSource { .. } | Load::Temperature { .. } => {}
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}
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}
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for (sid, loads) in &self.combinations {
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