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>
This commit is contained in:
authored and GitHub committed 2026-10-13 17:44:21 -04:00
1 parent 81fa8d7220
commit 40f98f0af9
33 files changed
+4559 -53

No files matched your search

+1
View File
@@ -14,6 +14,7 @@ modelcraft-geometry = { workspace = true }
modelcraft-mesh = { workspace = true }
modelcraft-io = { workspace = true }
modelcraft-decks = { workspace = true }
modelcraft-solver = { workspace = true }
serde = { workspace = true }
serde_json = { workspace = true }
thiserror = { workspace = true }
+4
View File
@@ -7,6 +7,7 @@ pub(crate) mod file;
mod geometry;
mod mesh;
mod model;
mod solve;
mod tags;
use modelcraft_model::MAX_LABEL;
@@ -68,6 +69,9 @@ pub static ALL: &[CommandSpec] = &[
edit::UNDO,
edit::REDO,
deck::WRITE,
solve::STATIC,
solve::FREQUENCY,
solve::PROBE,
];
/// A required label parameter (1..=u32::MAX; the model checks its own range).
+268
View File
@@ -0,0 +1,268 @@
//! `solve.*`: run the model's steps with the implicit solver, keep the results in the session,
//! and read them back.
use modelcraft_solver::{FrequencyOptions, Limits, MassKind, StepResult, solve_frequency, solve_static};
use serde_json::{Value, json};
use super::{labels, opt};
use crate::{CommandKind, CommandSpec, EngineError, Result, Session};
pub const STATIC: CommandSpec = CommandSpec {
id: "solve.static",
label: "Solve Static Step",
params: r#"{"step": "Load", "max_dofs": 6000000, "max_factor_entries": 400000000} — solves a linear static step (the only static step when `step` is left out) and keeps the result in the session; the caps may only be lowered"#,
kind: CommandKind::Model,
run: run_static,
};
pub const FREQUENCY: CommandSpec = CommandSpec {
id: "solve.frequency",
label: "Solve Frequency Step",
params: r#"{"step": "Modes", "mass": "consistent|lumped", "shift": 0.0, "max_dofs": 6000000, "max_factor_entries": 400000000, "max_iterations": 3000} — natural frequencies and mode shapes of a frequency step (its modes and range); `max_iterations` caps the Lanczos vectors; the result stays in the session"#,
kind: CommandKind::Model,
run: run_frequency,
};
pub const PROBE: CommandSpec = CommandSpec {
id: "solve.probe",
label: "Probe Results",
params: r#"{"step": "Load", "nodes": [1, 2], "mode": 1} — the stored result at nodes: displacement, reaction, stress and von Mises (static), or the shape of mode `mode` (frequency, from 1)"#,
kind: CommandKind::Model,
run: probe,
};
/// Most nodes one probe lists.
const MAX_PROBE: usize = 10_000;
/// An optional cap that may only lower the default.
fn cap(p: &Value, key: &str, default: usize) -> Result<usize> {
match p.get(key) {
None => Ok(default),
Some(v) => v
.as_u64()
.and_then(|n| usize::try_from(n).ok())
.filter(|n| (1..=default).contains(n))
.ok_or_else(|| EngineError::Params(format!("`{key}` must be a whole number from 1 to {default}"))),
}
}
fn limits(p: &Value) -> Result<Limits> {
Ok(Limits {
max_dofs: cap(p, "max_dofs", Limits::MAX_DOFS)?,
max_factor_entries: cap(p, "max_factor_entries", Limits::MAX_FACTOR_ENTRIES)?,
max_lanczos_vectors: cap(p, "max_iterations", Limits::MAX_LANCZOS_VECTORS)?,
})
}
fn largest(values: impl Iterator<Item = (u32, f64)>) -> Value {
match values.fold(None, |best: Option<(u32, f64)>, (l, v)| if best.is_none_or(|(_, b)| v > b) { Some((l, v)) } else { best }) {
Some((node, value)) => json!({"node": node, "value": value}),
None => Value::Null,
}
}
fn run_static(s: &mut Session, p: &Value) -> Result<Value> {
let limits = limits(p)?;
let step = opt::<String>(p, "step")?;
let r = solve_static(&s.model, step.as_deref(), &limits)?;
let magnitude = |u: &[f64; 3]| (u[0] * u[0] + u[1] * u[1] + u[2] * u[2]).sqrt();
let summary = json!({
"step": r.step,
"dofs": r.stats.dofs,
"equations": r.stats.equations,
"factor_entries": r.stats.factor_entries,
"max_displacement": largest(r.nodes.iter().zip(&r.displacement).map(|(l, u)| (*l, magnitude(u)))),
"max_von_mises": largest(r.nodes.iter().zip(&r.von_mises).map(|(l, v)| (*l, *v))),
"applied_total": r.applied_total,
"reaction_total": r.reaction_total,
"warnings": r.warnings,
});
s.store_result(StepResult::Static(r));
Ok(summary)
}
fn run_frequency(s: &mut Session, p: &Value) -> Result<Value> {
let limits = limits(p)?;
let step = opt::<String>(p, "step")?;
let mass = opt::<MassKind>(p, "mass")?.unwrap_or_default();
let shift = opt::<f64>(p, "shift")?;
let r = solve_frequency(&s.model, step.as_deref(), &FrequencyOptions { mass, shift }, &limits)?;
let summary = json!({
"step": r.step,
"dofs": r.stats.dofs,
"equations": r.stats.equations,
"lanczos_vectors": r.stats.lanczos_vectors,
"total_mass": r.total_mass,
"modes": r.modes.iter().enumerate().map(|(i, m)| json!({
"mode": i + 1,
"frequency": m.frequency,
"eigenvalue": m.eigenvalue,
"effective_mass": m.effective_mass,
})).collect::<Vec<_>>(),
"warnings": r.warnings,
});
s.store_result(StepResult::Frequency(r));
Ok(summary)
}
fn probe(s: &mut Session, p: &Value) -> Result<Value> {
let step = opt::<String>(p, "step")?.ok_or_else(|| EngineError::Params("`step` is required".into()))?;
let result = s.result(&step).ok_or_else(|| EngineError::Params(format!("step `{step}` has no result; solve it first")))?;
let nodes = labels(p, "nodes", MAX_PROBE)?;
let index = |label: u32| {
result.nodes().binary_search(&label).map_err(|_| EngineError::Params(format!("node {label} has no result (it belongs to no solved element)")))
};
let out: Vec<Value> = match result.as_ref() {
StepResult::Static(r) => nodes
.iter()
.map(|&l| {
let i = index(l)?;
Ok(json!({
"node": l,
"displacement": r.displacement.get(i),
"reaction": r.reaction.get(i),
"stress": r.stress.get(i),
"von_mises": r.von_mises.get(i),
}))
})
.collect::<Result<_>>()?,
StepResult::Frequency(r) => {
let mode = opt::<usize>(p, "mode")?.unwrap_or(1);
let m = mode
.checked_sub(1)
.and_then(|k| r.modes.get(k))
.ok_or_else(|| EngineError::Params(format!("`mode` must be from 1 to {}", r.modes.len())))?;
nodes.iter().map(|&l| Ok(json!({"node": l, "shape": m.shape.get(index(l)?)}))).collect::<Result<_>>()?
}
};
Ok(json!({"step": step, "nodes": out}))
}
#[cfg(test)]
pub(crate) mod tests {
use super::*;
/// A cantilever 10 × 1 × 1 of ten hex8 elements with incompatible modes, clamped at x = 0,
/// a total force of 1 down on the free end; a static and a frequency step.
pub(crate) fn cantilever(s: &mut Session) {
let mut script = Vec::new();
let label = |i: usize, j: usize, k: usize| 1 + i + 11 * (j + 2 * k);
for k in 0..2 {
for j in 0..2 {
for i in 0..11 {
script.push(json!({"command": "mesh.node.add", "params": {"label": label(i, j, k), "xyz": [i, j, k]}}));
}
}
}
for i in 0..10 {
let nodes = [
label(i, 0, 0),
label(i + 1, 0, 0),
label(i + 1, 1, 0),
label(i, 1, 0),
label(i, 0, 1),
label(i + 1, 0, 1),
label(i + 1, 1, 1),
label(i, 1, 1),
];
script.push(json!({"command": "mesh.element.add", "params": {"label": i + 1, "kind": "hex8", "nodes": nodes}}));
}
let root: Vec<usize> = (0..4).map(|n| label(0, n % 2, n / 2)).collect();
let tip: Vec<usize> = (0..4).map(|n| label(10, n % 2, n / 2)).collect();
script.extend([
json!({"command": "model.set.create", "params": {"name": "all", "elements": (1..=10).collect::<Vec<_>>()}}),
json!({"command": "model.set.create", "params": {"name": "root", "nodes": root}}),
json!({"command": "model.set.create", "params": {"name": "tip", "nodes": tip}}),
json!({"command": "model.material.create", "params": {"name": "Mat", "elastic": {"type": "isotropic", "young": 1000, "poisson": 0}, "density": 1}}),
json!({"command": "model.section.create", "params": {"name": "bar", "set": "all", "material": "Mat", "kind": {"type": "solid"}, "formulation": {"incompatible_modes": true}}}),
json!({"command": "model.boundary_condition.create", "params": {"name": "clamp", "type": "fixed", "target": {"set": "root"}}}),
json!({"command": "model.load.create", "params": {"name": "push", "type": "force", "target": {"set": "tip"}, "vector": [0, 0, -1]}}),
json!({"command": "model.step.create", "params": {"name": "Bend", "procedure": {"type": "static"}, "boundary_conditions": ["clamp"], "loads": ["push"]}}),
json!({"command": "model.step.create", "params": {"name": "Modes", "procedure": {"type": "frequency", "modes": 4}, "boundary_conditions": ["clamp"]}}),
]);
s.run_script(&Value::Array(script)).unwrap();
}
#[test]
fn solve_keep_and_probe_results() {
let mut s = Session::default();
cantilever(&mut s);
let journal = s.journal.len();
let r = s.execute("solve.static", &json!({})).unwrap();
assert_eq!(r["step"], "Bend");
// Euler–Bernoulli P L³ / (3 E I) = 4, plus shear; the clamp and one element through the
// depth keep it within a few percent.
let d = r["max_displacement"]["value"].as_f64().unwrap();
assert!((d - 4.024).abs() / 4.024 < 0.03, "{r}");
assert!((r["reaction_total"][2].as_f64().unwrap() - 1.0).abs() < 1e-9, "{r}");
assert_eq!(s.journal.len(), journal, "solving does not change the model");
let probe = s.execute("solve.probe", &json!({"step": "Bend", "nodes": [11, 1]})).unwrap();
assert!(probe["nodes"][0]["displacement"][2].as_f64().unwrap() < -3.8, "{probe}");
assert!(probe["nodes"][1]["reaction"][2].as_f64().unwrap() != 0.0, "{probe}");
let f = s.execute("solve.frequency", &json!({"mass": "lumped"})).unwrap();
assert_eq!(f["modes"].as_array().unwrap().len(), 4, "{f}");
let shape = s.execute("solve.probe", &json!({"step": "Modes", "nodes": [44], "mode": 2})).unwrap();
assert!(shape["nodes"][0]["shape"].is_array(), "{shape}");
assert_eq!(s.solved_steps().count(), 2);
// Results describe the model they were solved for: an edit clears them, a failed command
// keeps them.
assert!(s.execute("model.material.edit", &json!({"name": "Mat", "elastic": {"type": "isotropic", "young": -1}})).is_err());
assert_eq!(s.solved_steps().count(), 2);
s.execute("model.material.edit", &json!({"name": "Mat", "elastic": {"type": "isotropic", "young": 2000, "poisson": 0}, "density": 1}))
.unwrap();
assert_eq!(s.solved_steps().count(), 0);
// Undo returns to the solved state, and its results are current again.
s.execute("edit.undo", &json!({})).unwrap();
assert_eq!(s.solved_steps().count(), 2);
s.execute("edit.redo", &json!({})).unwrap();
assert!(s.execute("solve.probe", &json!({"step": "Bend", "nodes": [1]})).is_err());
}
#[test]
fn solve_hostile_params_never_panic() {
let mut s = Session::default();
cantilever(&mut s);
s.execute("solve.static", &json!({})).unwrap();
s.execute("solve.frequency", &json!({})).unwrap();
let hostile = [
json!(null),
json!({"step": 7}),
json!({"step": "Nope"}),
json!({"step": "Modes"}),
json!({"step": "Bend", "max_dofs": 0}),
json!({"step": "Bend", "max_dofs": 1e300}),
json!({"step": "Bend", "max_dofs": 3}),
json!({"step": "Bend", "max_factor_entries": -1}),
json!({"step": "Bend", "max_factor_entries": 10}),
json!({"step": "Modes", "max_iterations": 1}),
json!({"step": "Modes", "max_iterations": 7}),
json!({"step": "Modes", "mass": "heavy"}),
json!({"step": "Modes", "shift": 1e308}),
json!({"step": "Modes", "shift": -1e308}),
json!({"step": "Modes", "shift": 5000.0}),
json!({"step": "Modes", "shift": "x"}),
json!({"step": "Modes", "nodes": [1], "mode": 0}),
json!({"step": "Modes", "nodes": [1], "mode": 1e300}),
json!({"step": "Bend", "nodes": [0, 99999999, 4294967296u64]}),
json!({"step": "Bend", "nodes": vec![1; 20_000]}),
];
for id in ["solve.static", "solve.frequency", "solve.probe"] {
for p in &hostile {
let mut t = s.clone();
let before = t.model.clone();
let results = t.solved_steps().count();
if t.execute(id, p).is_err() {
assert_eq!(t.model, before);
assert_eq!(t.solved_steps().count(), results, "{id} {p}");
}
}
}
// An unsupported model (a coupling, a reference point load) is an error, not a panic.
let mut defined = Session::default();
crate::cmd::define::tests::defined_bar(&mut defined);
let e = defined.execute("solve.static", &json!({"step": "Bend"})).unwrap_err().to_string();
assert!(e.contains("not supported yet"), "{e}");
}
}
+23
View File
@@ -17,11 +17,13 @@ pub mod cmd;
pub mod history;
pub mod sample;
use std::collections::BTreeMap;
use std::sync::Arc;
use modelcraft_geometry::Design;
use modelcraft_geometry::tagged_mesh::TaggedSurface;
use modelcraft_model::Model;
use modelcraft_solver::StepResult;
use serde_json::Value;
use crate::history::History;
@@ -42,6 +44,8 @@ pub enum EngineError {
File(#[from] modelcraft_io::Error),
#[error(transparent)]
Deck(#[from] modelcraft_decks::Error),
#[error(transparent)]
Solver(#[from] modelcraft_solver::Error),
/// A command panicked; the model is unchanged.
#[error("internal error in {command}: {message}")]
Internal { command: String, message: String },
@@ -110,6 +114,9 @@ pub struct Session {
/// The revision last saved to (or opened from) `path`; `None` when the content was never
/// saved, where only the empty start (revision 0) is clean.
saved_revision: Option<u64>,
/// The latest result of each solved step, by step name, with the revision it was solved at;
/// [`Session::result`] hands out only those that describe the current state.
results: BTreeMap<String, (u64, Arc<StepResult>)>,
}
impl Session {
@@ -163,6 +170,22 @@ impl Session {
self.saved_revision.unwrap_or(0) != self.revision
}
/// The stored result of a step, if it was solved in the current state (an edit makes it stale;
/// undoing back to the solved state makes it current again).
pub fn result(&self, step: &str) -> Option<&Arc<StepResult>> {
self.results.get(step).filter(|(revision, _)| *revision == self.revision).map(|(_, r)| r)
}
/// The steps with a current result.
pub fn solved_steps(&self) -> impl Iterator<Item = &str> {
self.results.iter().filter(|(_, (revision, _))| *revision == self.revision).map(|(name, _)| name.as_str())
}
/// Keep a step's result for the current state.
pub(crate) fn store_result(&mut self, result: StepResult) {
self.results.insert(result.step().to_string(), (self.revision, Arc::new(result)));
}
/// The current state is what `path` now holds.
pub(crate) fn mark_saved(&mut self, path: String) {
self.path = Some(path);
+13
View File
@@ -0,0 +1,13 @@
[package]
name = "modelcraft-fem"
description = "ModelCraft's finite element kernels: shape functions, quadrature, strain-displacement matrices, element stiffness and mass, elastic constitutive matrices"
version.workspace = true
edition.workspace = true
license.workspace = true
[lints]
workspace = true
[dependencies]
modelcraft-model = { workspace = true }
thiserror = { workspace = true }
+138
View File
@@ -0,0 +1,138 @@
//! Small dense matrices: element matrices and the little systems inside an element (static
//! condensation, extrapolation fits).
use crate::{Error, Result};
/// A square matrix, row-major.
#[derive(Debug, Clone, PartialEq)]
pub struct Matrix {
pub n: usize,
pub data: Vec<f64>,
}
impl Matrix {
pub fn zeros(n: usize) -> Matrix {
Matrix { n, data: vec![0.0; n * n] }
}
pub fn get(&self, i: usize, j: usize) -> f64 {
self.data.get(i * self.n + j).copied().unwrap_or(0.0)
}
pub fn add(&mut self, i: usize, j: usize, v: f64) {
if let Some(x) = self.data.get_mut(i * self.n + j) {
*x += v;
}
}
/// y = A x (x shorter than n is padded with zeros).
pub fn mul_vec(&self, x: &[f64]) -> Vec<f64> {
self.data.chunks_exact(self.n.max(1)).map(|row| row.iter().zip(x).map(|(a, b)| a * b).sum()).collect()
}
}
/// The Cholesky factor of a small symmetric positive definite matrix (lower triangle, row-major).
#[derive(Debug, Clone)]
pub struct Cholesky {
n: usize,
l: Vec<f64>,
}
impl Cholesky {
/// Factor `a` (only its lower triangle is read). Fails when a pivot is not positive relative
/// to the matrix's diagonal.
pub fn new(a: &Matrix) -> Result<Cholesky> {
let n = a.n;
let mut l = vec![0.0; n * n];
let scale = (0..n).map(|i| a.get(i, i).abs()).fold(0.0, f64::max);
for j in 0..n {
let mut d = a.get(j, j);
for k in 0..j {
let v = l[j * n + k];
d -= v * v;
}
if !(d > 1e-13 * scale) {
return Err(Error::Singular(format!("a {n} × {n} element matrix is not positive definite (pivot {j})")));
}
let djj = d.sqrt();
l[j * n + j] = djj;
for i in j + 1..n {
let mut s = a.get(i, j);
for k in 0..j {
s -= l[i * n + k] * l[j * n + k];
}
l[i * n + j] = s / djj;
}
}
Ok(Cholesky { n, l })
}
/// Solve A x = b in place.
pub fn solve(&self, b: &mut [f64]) {
let n = self.n.min(b.len());
for i in 0..n {
let mut s = b[i];
for k in 0..i {
s -= self.l[i * self.n + k] * b[k];
}
b[i] = s / self.l[i * self.n + i];
}
for i in (0..n).rev() {
let mut s = b[i];
for k in i + 1..n {
s -= self.l[k * self.n + i] * b[k];
}
b[i] = s / self.l[i * self.n + i];
}
}
}
/// The inverse and determinant of a 3 × 3 matrix; `None` when it is singular or not finite.
pub fn inverse3(m: &[[f64; 3]; 3]) -> Option<([[f64; 3]; 3], f64)> {
let det = det3(m);
if !(det.abs() > 0.0 && det.is_finite()) {
return None;
}
let mut inv = [[0.0; 3]; 3];
for (i, row) in inv.iter_mut().enumerate() {
for (j, v) in row.iter_mut().enumerate() {
let (j1, j2) = ((j + 1) % 3, (j + 2) % 3);
let (i1, i2) = ((i + 1) % 3, (i + 2) % 3);
// inv[i][j] = cofactor[j][i] / det.
*v = (m[j1][i1] * m[j2][i2] - m[j1][i2] * m[j2][i1]) / det;
}
}
Some((inv, det))
}
pub fn det3(m: &[[f64; 3]; 3]) -> f64 {
m[0][0] * (m[1][1] * m[2][2] - m[1][2] * m[2][1]) - m[0][1] * (m[1][0] * m[2][2] - m[1][2] * m[2][0])
+ m[0][2] * (m[1][0] * m[2][1] - m[1][1] * m[2][0])
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn cholesky_solves_and_rejects_indefinite() {
let mut a = Matrix::zeros(3);
a.data = vec![4.0, 2.0, 0.6, 2.0, 5.0, 1.0, 0.6, 1.0, 3.0];
let x = [1.0, -2.0, 0.5];
let mut b = a.mul_vec(&x);
Cholesky::new(&a).unwrap().solve(&mut b);
assert!(b.iter().zip(x).all(|(p, q)| (p - q).abs() < 1e-14), "{b:?}");
a.data[8] = -1.0;
assert!(Cholesky::new(&a).is_err());
let m = [[2.0, 0.5, 0.0], [0.1, 3.0, 0.2], [0.0, 0.4, 1.0]];
let (inv, det) = inverse3(&m).unwrap();
assert!((det - det3(&m)).abs() < 1e-15);
for i in 0..3 {
for j in 0..3 {
let p: f64 = (0..3).map(|k| m[i][k] * inv[k][j]).sum();
assert!((p - if i == j { 1.0 } else { 0.0 }).abs() < 1e-14);
}
}
assert!(inverse3(&[[1.0, 2.0, 3.0], [2.0, 4.0, 6.0], [0.0, 0.0, 1.0]]).is_none());
}
}
+610
View File
@@ -0,0 +1,610 @@
//! Solid continuum elements: the element table, stiffness, mass, body forces, stresses at the
//! integration points and their extrapolation to the nodes.
//!
//! The isoparametric displacement formulation (Zienkiewicz, Taylor & Zhu 2013, ch. 6; Hughes
//! 2000, ch. 3): K = ∫ Bᵀ D B dV and M = ∫ ρ Nᵀ N dV, integrated by Gauss quadrature on the
//! reference element through the Jacobian of the map from natural to physical coordinates.
//!
//! Formulations:
//! - **full integration**: the rule that integrates the stiffness of an undistorted element
//! exactly (1 point for tet4, 4 for tet10, 2 × 2 × 2 for hex8, 3 × 3 × 3 for hex20);
//! - **reduced integration** for hex20 (2 × 2 × 2), which avoids locking at the cost of one
//! spurious mode that a mesh of more than one element restrains. Reduced hex8 needs hourglass
//! control and is not offered here yet (it arrives with the explicit solver, Flanagan &
//! Belytschko 1981);
//! - **incompatible modes** for hex8 (E. L. Wilson, R. L. Taylor, W. P. Doherty, J. Ghaboussi,
//! *Incompatible displacement models*, in Numerical and Computer Methods in Structural
//! Mechanics, Academic Press 1973, 43–57): nine internal displacement modes (1 − ξ²),
//! (1 − η²), (1 − ζ²) per direction, condensed out of the element. Their derivatives use the
//! Jacobian at the element centre scaled by det J₀ / det J, the correction of R. L. Taylor,
//! P. J. Beresford, E. L. Wilson, *A non-conforming element for stress analysis*, IJNME
//! 10(6):1211–1219, 1976, so the element passes the patch test when distorted. It bends
//! correctly with one element through the thickness.
//!
//! Lumped mass is the diagonal scaling of Hinton, Rock and Zienkiewicz (E. Hinton, T. Rock,
//! O. C. Zienkiewicz, *A note on mass lumping and related processes in the finite element
//! method*, Earthquake Eng. Struct. Dyn. 4(3):245–249, 1976): the consistent diagonal scaled to
//! the element's mass, positive for quadratic elements too.
//!
//! Nodal stresses extrapolate the integration-point values with the element's linear corner
//! functions fitted by least squares (E. Hinton, J. S. Campbell, *Local and global smoothing of
//! discontinuous finite element functions using a least squares method*, IJNME 8(3):461–480,
//! 1974); mid-side nodes take the mean of their edge's corners.
use modelcraft_model::ElementKind;
use crate::dense::{Cholesky, Matrix, inverse3};
use crate::material::{Elasticity, stress};
use crate::quadrature::{Point, Rule};
use crate::shape::{self, MAX_NODES, Shape};
use crate::{Error, Result};
/// The reference shape of an element type.
#[derive(Debug, Clone, Copy, PartialEq, Eq)]
pub enum Family {
Tetrahedron,
Hexahedron,
}
/// One row of the element table: everything the kernels need to know about an element kind.
/// Adding an element (wedge6, shells, beams) is adding a row and its shape functions.
#[derive(Debug)]
pub struct ElementType {
pub kind: ElementKind,
pub family: Family,
pub nodes: usize,
/// The corner nodes come first in the node list.
pub corners: usize,
pub shape: fn([f64; 3]) -> Shape,
/// Full integration of the stiffness.
pub full: Rule,
/// Reduced integration, where the element is stable with it.
pub reduced: Option<Rule>,
/// Exact for the consistent mass of an undistorted element.
pub mass: Rule,
/// Whether the element has an incompatible-modes formulation.
pub incompatible_modes: bool,
}
/// The element table.
pub static ELEMENT_TYPES: [ElementType; 4] = [
ElementType {
kind: ElementKind::Tet4,
family: Family::Tetrahedron,
nodes: 4,
corners: 4,
shape: shape::tet4,
full: Rule::TetCentroid,
reduced: None,
mass: Rule::Tet4,
incompatible_modes: false,
},
ElementType {
kind: ElementKind::Tet10,
family: Family::Tetrahedron,
nodes: 10,
corners: 4,
shape: shape::tet10,
full: Rule::Tet4,
reduced: None,
mass: Rule::TetConical(4),
incompatible_modes: false,
},
ElementType {
kind: ElementKind::Hex8,
family: Family::Hexahedron,
nodes: 8,
corners: 8,
shape: shape::hex8,
full: Rule::Hex(2),
reduced: None,
mass: Rule::Hex(2),
incompatible_modes: true,
},
ElementType {
kind: ElementKind::Hex20,
family: Family::Hexahedron,
nodes: 20,
corners: 8,
shape: shape::hex20,
full: Rule::Hex(3),
reduced: Some(Rule::Hex(2)),
mass: Rule::Hex(3),
incompatible_modes: false,
},
];
/// The table row of an element kind.
pub fn element_type(kind: ElementKind) -> Result<&'static ElementType> {
ELEMENT_TYPES
.iter()
.find(|t| t.kind == kind)
.ok_or_else(|| Error::NotSupported(format!("{} elements (the solver has tet4, tet10, hex8 and hex20 so far)", kind.name())))
}
/// How a solid element is formulated.
#[derive(Debug, Clone, Copy, PartialEq, Eq)]
pub enum Formulation {
Full,
Reduced,
IncompatibleModes,
}
impl Formulation {
/// The formulation a model section asks for, if this element type has it.
pub fn from_section(kind: ElementKind, f: &modelcraft_model::Formulation) -> Result<Formulation> {
let ty = element_type(kind)?;
if f.hybrid {
return Err(Error::NotSupported("hybrid (mixed displacement–pressure) elements".into()));
}
if f.incompatible_modes {
return if ty.incompatible_modes {
Ok(Formulation::IncompatibleModes)
} else {
Err(Error::Invalid(format!("incompatible modes apply to hex8 elements, not {}", kind.name())))
};
}
match f.integration {
modelcraft_model::Integration::Full => Ok(Formulation::Full),
modelcraft_model::Integration::Reduced if ty.reduced.is_some() => Ok(Formulation::Reduced),
modelcraft_model::Integration::Reduced => Err(Error::NotSupported(format!(
"reduced integration of {} elements (hex8 needs hourglass control; use full integration or incompatible modes)",
kind.name()
))),
}
}
}
/// Strain, stress and position at one integration point.
#[derive(Debug, Clone, Copy, PartialEq)]
pub struct PointStress {
pub xyz: [f64; 3],
pub strain: [f64; 6],
pub stress: [f64; 6],
}
/// Shape function gradients in physical coordinates at one point.
struct Gradients {
shape: Shape,
dx: [[f64; 3]; MAX_NODES],
det: f64,
}
/// A solid element: its type, its node coordinates and its formulation.
#[derive(Debug, Clone, Copy)]
pub struct Solid<'a> {
pub ty: &'static ElementType,
xyz: &'a [[f64; 3]],
formulation: Formulation,
}
/// The stiffness blocks of the incompatible-modes element.
struct IncompatibleParts {
kuu: Matrix,
kua: Vec<f64>,
kaa: Matrix,
j0: ([[f64; 3]; 3], f64),
}
/// The incompatible modes' count of internal degrees of freedom.
const INCOMPATIBLE_DOFS: usize = 9;
impl<'a> Solid<'a> {
pub fn new(kind: ElementKind, xyz: &'a [[f64; 3]], formulation: Formulation) -> Result<Solid<'a>> {
let ty = element_type(kind)?;
if xyz.len() != ty.nodes {
return Err(Error::Invalid(format!("a {} element has {} nodes, got {}", kind.name(), ty.nodes, xyz.len())));
}
modelcraft_model::check_coordinates(xyz.as_flattened()).map_err(|e| Error::Invalid(e.to_string()))?;
let ok = match formulation {
Formulation::Full => true,
Formulation::Reduced => ty.reduced.is_some(),
Formulation::IncompatibleModes => ty.incompatible_modes,
};
if !ok {
return Err(Error::NotSupported(format!("{formulation:?} formulation of {} elements", kind.name())));
}
Ok(Solid { ty, xyz, formulation })
}
/// The stiffness integration rule.
pub fn rule(&self) -> Rule {
match (self.formulation, self.ty.reduced) {
(Formulation::Reduced, Some(r)) => r,
_ => self.ty.full,
}
}
/// The stiffness integration points (where stresses are reported).
pub fn integration_points(&self) -> Vec<Point> {
self.rule().points()
}
/// The Jacobian matrix J[a][b] = ∂x_b/∂ξ_a.
fn jacobian(&self, s: &Shape) -> [[f64; 3]; 3] {
let mut j = [[0.0; 3]; 3];
for (d, x) in s.derivatives().iter().zip(self.xyz) {
for a in 0..3 {
for b in 0..3 {
j[a][b] += d[a] * x[b];
}
}
}
j
}
fn gradients(&self, xi: [f64; 3]) -> Result<Gradients> {
let shape = (self.ty.shape)(xi);
let j = self.jacobian(&shape);
let (inv, det) = inverse3(&j).ok_or_else(|| self.degenerate())?;
let norms: f64 = j.iter().map(|r| (r[0] * r[0] + r[1] * r[1] + r[2] * r[2]).sqrt()).product();
if !(det > 1e-12 * norms) {
return Err(self.degenerate());
}
let mut dx = [[0.0; 3]; MAX_NODES];
for (g, d) in dx.iter_mut().zip(shape.derivatives()) {
for b in 0..3 {
g[b] = inv[b][0] * d[0] + inv[b][1] * d[1] + inv[b][2] * d[2];
}
}
Ok(Gradients { shape, dx, det })
}
fn degenerate(&self) -> Error {
Error::Degenerate(format!("a {} element is inverted or degenerate (its Jacobian is not positive)", self.ty.kind.name()))
}
/// Position of a natural point.
pub fn position(&self, xi: [f64; 3]) -> [f64; 3] {
let s = (self.ty.shape)(xi);
let mut p = [0.0; 3];
for (n, x) in s.values().iter().zip(self.xyz) {
for k in 0..3 {
p[k] += n * x[k];
}
}
p
}
/// The element's volume.
pub fn volume(&self) -> Result<f64> {
let mut v = 0.0;
for p in self.ty.mass.points() {
v += self.gradients(p.xi)?.det * p.weight;
}
Ok(v)
}
/// The incompatible modes' gradients at a point: det J₀/det J · J₀⁻¹ ∂P/∂ξ.
fn incompatible_gradients(&self, xi: [f64; 3], det: f64, j0: &([[f64; 3]; 3], f64)) -> [[f64; 3]; 3] {
let (inv0, det0) = j0;
let mut g = [[0.0; 3]; 3];
for (k, gk) in g.iter_mut().enumerate() {
// ∂(1 − ξ_k²)/∂ξ_k = −2 ξ_k, other derivatives zero.
let dp = -2.0 * xi[k];
for b in 0..3 {
gk[b] = det0 / det * inv0[b][k] * dp;
}
}
g
}
fn centre_jacobian(&self) -> Result<([[f64; 3]; 3], f64)> {
let s = (self.ty.shape)([0.0; 3]);
inverse3(&self.jacobian(&s)).filter(|(_, d)| *d > 0.0).ok_or_else(|| self.degenerate())
}
/// The parts of the stiffness with the incompatible modes: K_uu (when `with_uu`), K_ua
/// (3n × 9), K_aa, and the centre Jacobian they were built with.
fn incompatible_parts(&self, d: &Elasticity, with_uu: bool) -> Result<IncompatibleParts> {
let n = 3 * self.ty.nodes;
let j0 = self.centre_jacobian()?;
let mut kuu = Matrix::zeros(if with_uu { n } else { 0 });
let mut kua = vec![0.0; n * INCOMPATIBLE_DOFS];
let mut kaa = Matrix::zeros(INCOMPATIBLE_DOFS);
for p in self.rule().points() {
let g = self.gradients(p.xi)?;
let w = g.det * p.weight;
let ga = self.incompatible_gradients(p.xi, g.det, &j0);
let gu = g.dx.get(..self.ty.nodes).unwrap_or_default();
if with_uu {
accumulate_symmetric(&mut kuu.data, gu, d, w);
}
accumulate(&mut kua, INCOMPATIBLE_DOFS, gu, &ga, d, w);
accumulate_symmetric(&mut kaa.data, &ga, d, w);
}
Ok(IncompatibleParts { kuu, kua, kaa, j0 })
}
/// The stiffness matrix, 3n × 3n, degrees of freedom ordered node by node (x, y, z).
pub fn stiffness(&self, d: &Elasticity) -> Result<Matrix> {
let n = 3 * self.ty.nodes;
if self.formulation == Formulation::IncompatibleModes {
let IncompatibleParts { kuu: mut k, kua, kaa, .. } = self.incompatible_parts(d, true)?;
let chol = Cholesky::new(&kaa)?;
// K = K_uu − K_ua K_aa⁻¹ K_au, column by column of K_au.
for i in 0..n {
let mut col: Vec<f64> = kua.get(i * INCOMPATIBLE_DOFS..(i + 1) * INCOMPATIBLE_DOFS).unwrap_or_default().to_vec();
chol.solve(&mut col);
for j in 0..n {
let row = kua.get(j * INCOMPATIBLE_DOFS..(j + 1) * INCOMPATIBLE_DOFS).unwrap_or_default();
let v: f64 = row.iter().zip(&col).map(|(a, b)| a * b).sum();
k.add(j, i, -v);
}
}
symmetrize(&mut k);
return Ok(k);
}
let mut k = Matrix::zeros(n);
for p in self.rule().points() {
let g = self.gradients(p.xi)?;
let gu = g.dx.get(..self.ty.nodes).unwrap_or_default();
accumulate_symmetric(&mut k.data, gu, d, g.det * p.weight);
}
Ok(k)
}
/// The consistent mass matrix per displacement component, n × n: m_ij = ∫ ρ Nᵢ Nⱼ dV (the
/// 3n × 3n matrix has it on each component's block).
pub fn mass(&self, density: f64) -> Result<Matrix> {
let n = self.ty.nodes;
let mut m = Matrix::zeros(n);
for p in self.ty.mass.points() {
let g = self.gradients(p.xi)?;
let w = density * g.det * p.weight;
let v = g.shape.values();
for (i, a) in v.iter().enumerate() {
for (j, b) in v.iter().enumerate() {
m.add(i, j, w * a * b);
}
}
}
Ok(m)
}
/// The lumped (diagonal) mass per node: the consistent diagonal scaled to the element's mass.
pub fn lumped_mass(&self, density: f64) -> Result<Vec<f64>> {
let m = self.mass(density)?;
// The consistent entries sum to the element's mass (the shape functions sum to one).
let total: f64 = m.data.iter().sum();
let diag: Vec<f64> = (0..m.n).map(|i| m.get(i, i)).collect();
let sum: f64 = diag.iter().sum();
if !(sum > 0.0) {
return Err(self.degenerate());
}
Ok(diag.iter().map(|d| d * total / sum).collect())
}
/// Consistent nodal forces of a uniform force per volume: fᵢ = ∫ Nᵢ b dV.
pub fn body_force(&self, b: [f64; 3]) -> Result<Vec<[f64; 3]>> {
let mut f = vec![[0.0; 3]; self.ty.nodes];
for p in self.ty.mass.points() {
let g = self.gradients(p.xi)?;
for (fi, n) in f.iter_mut().zip(g.shape.values()) {
for k in 0..3 {
fi[k] += n * b[k] * g.det * p.weight;
}
}
}
Ok(f)
}
/// Strain and stress at every integration point for the nodal displacements `u`.
pub fn stresses(&self, d: &Elasticity, u: &[[f64; 3]]) -> Result<Vec<PointStress>> {
if u.len() != self.ty.nodes {
return Err(Error::Invalid(format!("{} displacements for a {}-node element", u.len(), self.ty.nodes)));
}
// Incompatible modes: recover the internal amplitudes α = −K_aa⁻¹ K_au u.
let alpha = if self.formulation == Formulation::IncompatibleModes {
let IncompatibleParts { kua, kaa, j0, .. } = self.incompatible_parts(d, false)?;
let flat: Vec<f64> = u.iter().flatten().copied().collect();
let mut rhs = [0.0; INCOMPATIBLE_DOFS];
for (i, ui) in flat.iter().enumerate() {
for (a, r) in rhs.iter_mut().enumerate() {
*r -= kua.get(i * INCOMPATIBLE_DOFS + a).copied().unwrap_or(0.0) * ui;
}
}
Cholesky::new(&kaa)?.solve(&mut rhs);
Some((rhs, j0))
} else {
None
};
let mut out = Vec::new();
for p in self.rule().points() {
let g = self.gradients(p.xi)?;
let mut grad = [[0.0; 3]; 3]; // ∂u_c/∂x_b
for (dn, ui) in g.dx.iter().zip(u) {
for c in 0..3 {
for b in 0..3 {
grad[c][b] += ui[c] * dn[b];
}
}
}
if let Some((a, j0)) = &alpha {
let ga = self.incompatible_gradients(p.xi, g.det, j0);
for (k, gk) in ga.iter().enumerate() {
for c in 0..3 {
for b in 0..3 {
grad[c][b] += a[3 * k + c] * gk[b];
}
}
}
}
let strain = [grad[0][0], grad[1][1], grad[2][2], grad[0][1] + grad[1][0], grad[0][2] + grad[2][0], grad[1][2] + grad[2][1]];
let mut xyz = [0.0; 3];
for (n, x) in g.shape.values().iter().zip(self.xyz) {
for k in 0..3 {
xyz[k] += n * x[k];
}
}
out.push(PointStress { xyz, strain, stress: stress(d, &strain) });
}
Ok(out)
}
/// Extrapolate values at the integration points to the element's nodes.
pub fn extrapolate(&self, values: &[[f64; 6]]) -> Result<Vec<[f64; 6]>> {
let e = extrapolation(self.ty, self.rule())?;
if values.len() != e.points {
return Err(Error::Invalid(format!("{} values for {} integration points", values.len(), e.points)));
}
Ok(e.apply(values))
}
}
/// Make a matrix exactly symmetric (the mean of it and its transpose), so assembly can rely on it.
fn symmetrize(k: &mut Matrix) {
let n = k.n;
for i in 0..n {
for j in i + 1..n {
let v = 0.5 * (k.get(i, j) + k.get(j, i));
if let Some(x) = k.data.get_mut(i * n + j) {
*x = v;
}
if let Some(x) = k.data.get_mut(j * n + i) {
*x = v;
}
}
}
}
/// The strain-displacement block of one gradient g: ε = B u for a single node's (x, y, z).
fn b_block(g: &[f64; 3]) -> [[f64; 3]; 6] {
[[g[0], 0.0, 0.0], [0.0, g[1], 0.0], [0.0, 0.0, g[2]], [g[1], g[0], 0.0], [g[2], 0.0, g[0]], [0.0, g[2], g[1]]]
}
/// out[3i + r][3j + c] += w (Bᵢᵀ D Bⱼ)[r][c] for gradients `ga` (rows) and `gb` (columns), with
/// `cols` columns in the row-major `out`.
fn accumulate(out: &mut [f64], cols: usize, ga: &[[f64; 3]], gb: &[[f64; 3]], d: &Elasticity, w: f64) {
for (j, gj) in gb.iter().enumerate() {
let bj = b_block(gj);
// D Bⱼ: 6 × 3.
let mut db = [[0.0; 3]; 6];
for s in 0..6 {
for c in 0..3 {
db[s][c] = (0..6).map(|t| d[s][t] * bj[t][c]).sum();
}
}
for (i, gi) in ga.iter().enumerate() {
let bi = b_block(gi);
for r in 0..3 {
for c in 0..3 {
let v: f64 = (0..6).map(|s| bi[s][r] * db[s][c]).sum();
if let Some(x) = out.get_mut((3 * i + r) * cols + 3 * j + c) {
*x += w * v;
}
}
}
}
}
}
/// The symmetric case of [`accumulate`] (rows and columns from the same gradients, `out` square):
/// computes the blocks with j ≥ i and mirrors them, so the result is exactly symmetric.
fn accumulate_symmetric(out: &mut [f64], g: &[[f64; 3]], d: &Elasticity, w: f64) {
let cols = 3 * g.len();
for (j, gj) in g.iter().enumerate() {
let bj = b_block(gj);
let mut db = [[0.0; 3]; 6];
for s in 0..6 {
for c in 0..3 {
db[s][c] = (0..6).map(|t| d[s][t] * bj[t][c]).sum();
}
}
for (i, gi) in g.iter().enumerate().take(j + 1) {
let bi = b_block(gi);
for r in 0..3 {
// On a diagonal block only the upper triangle is computed, then mirrored.
for c in if i == j { r } else { 0 }..3 {
let v = w * (0..6).map(|s| bi[s][r] * db[s][c]).sum::<f64>();
let (row, col) = (3 * i + r, 3 * j + c);
if let Some(x) = out.get_mut(row * cols + col) {
*x += v;
}
if row != col
&& let Some(x) = out.get_mut(col * cols + row)
{
*x += v;
}
}
}
}
}
}
/// The map from integration-point values to nodal values of an element type and rule.
#[derive(Debug, Clone)]
pub struct Extrapolation {
pub points: usize,
/// nodes × points, row-major.
pub weights: Vec<f64>,
}
impl Extrapolation {
pub fn apply(&self, values: &[[f64; 6]]) -> Vec<[f64; 6]> {
self.weights
.chunks_exact(self.points.max(1))
.map(|row| {
let mut v = [0.0; 6];
for (w, x) in row.iter().zip(values) {
for k in 0..6 {
v[k] += w * x[k];
}
}
v
})
.collect()
}
}
/// The least-squares extrapolation of a rule's points to the nodes with the linear corner
/// functions (Hinton & Campbell 1974); the mean when the rule has fewer points than corners.
pub fn extrapolation(ty: &ElementType, rule: Rule) -> Result<Extrapolation> {
let pts = rule.points();
let g = pts.len();
let c = ty.corners;
let corner_basis = |xi: [f64; 3]| match ty.family {
Family::Tetrahedron => shape::tet4(xi),
Family::Hexahedron => shape::hex8(xi),
};
let mut corner_rows = vec![0.0; c * g];
if g < c {
corner_rows.iter_mut().for_each(|w| *w = 1.0 / g.max(1) as f64);
} else {
// (AᵀA)⁻¹ Aᵀ with A[p][j] = corner function j at point p.
let a: Vec<Vec<f64>> = pts.iter().map(|p| corner_basis(p.xi).values().to_vec()).collect();
let mut ata = Matrix::zeros(c);
for row in &a {
for i in 0..c {
for j in 0..c {
ata.add(i, j, row.get(i).copied().unwrap_or(0.0) * row.get(j).copied().unwrap_or(0.0));
}
}
}
let chol = Cholesky::new(&ata)?;
for (p, row) in a.iter().enumerate() {
let mut col = row.clone();
chol.solve(&mut col);
for (i, v) in col.iter().enumerate() {
if let Some(x) = corner_rows.get_mut(i * g + p) {
*x = *v;
}
}
}
}
let mut weights = vec![0.0; ty.nodes * g];
for (w, v) in weights.iter_mut().zip(&corner_rows) {
*w = *v;
}
for edge in ty.kind.edges() {
if let [a, b, m] = **edge {
for p in 0..g {
let v = 0.5 * (corner_rows.get(a * g + p).copied().unwrap_or(0.0) + corner_rows.get(b * g + p).copied().unwrap_or(0.0));
if let Some(x) = weights.get_mut(m * g + p) {
*x = v;
}
}
}
}
Ok(Extrapolation { points: g, weights })
}
+76
View File
@@ -0,0 +1,76 @@
//! Element faces: consistent nodal forces of surface loads.
//!
//! A pressure p on a face gives node i the force fᵢ = −p ∫ Nᵢ n dA, where n dA =
//! (∂x/∂ξ × ∂x/∂η) dξ dη on the face's own, possibly curved, geometry; faces are numbered so this
//! normal points out of the element ([`modelcraft_model::ElementKind::faces`]), and a positive
//! pressure pushes in. This is the consistent load vector of the virtual work of the surface load
//! (Zienkiewicz, Taylor & Zhu 2013, §6.6), integrated with the model's face rules (exact for a
//! uniform pressure on a flat face).
use crate::{Error, Result};
/// ∫ Nᵢ n dA for every node of a face (node coordinates in the face's node order): the model's
/// face integration ([`modelcraft_model::nodal::face_normal_weights`]), so pressures and the
/// tractions the model distributes use the same rule.
pub fn normal_weights(xyz: &[[f64; 3]]) -> Result<Vec<[f64; 3]>> {
modelcraft_model::nodal::face_normal_weights(xyz).map_err(|e| Error::Invalid(e.to_string()))
}
/// Consistent nodal forces of a uniform pressure (positive pushes into the element).
pub fn pressure(xyz: &[[f64; 3]], magnitude: f64) -> Result<Vec<[f64; 3]>> {
Ok(normal_weights(xyz)?.into_iter().map(|w| w.map(|c| -magnitude * c)).collect())
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn pressure_on_flat_faces_is_the_textbook_split() {
// A 2 × 3 quadrilateral in z = 0, normal +z: quad4 shares p A equally, quad8 gives the
// corners −A/12 and the mid-sides A/3.
let quad = [[0., 0., 0.], [2., 0., 0.], [2., 3., 0.], [0., 3., 0.]];
let f = pressure(&quad, 1.0).unwrap();
assert!(f.iter().all(|v| (v[2] + 1.5).abs() < 1e-14 && v[0] == 0.0 && v[1] == 0.0), "{f:?}");
let mut q8 = quad.to_vec();
for (a, b) in [(0, 1), (1, 2), (2, 3), (3, 0)] {
q8.push([0, 1, 2].map(|k| (quad[a][k] + quad[b][k]) / 2.0));
}
let f = pressure(&q8, 1.0).unwrap();
for (i, v) in f.iter().enumerate() {
let want = if i < 4 { 0.5 } else { -2.0 };
assert!((v[2] - want).abs() < 1e-13, "{i}: {v:?}");
}
// Triangles: tri3 A/3 each; tri6 corners 0, mid-sides A/3.
let tri = [[0., 0., 0.], [1., 0., 0.], [0., 1., 0.]];
let f = pressure(&tri, 6.0).unwrap();
assert!(f.iter().all(|v| (v[2] + 1.0).abs() < 1e-14), "{f:?}");
let mut t6 = tri.to_vec();
for (a, b) in [(0, 1), (1, 2), (2, 0)] {
t6.push([0, 1, 2].map(|k| (tri[a][k] + tri[b][k]) / 2.0));
}
let f = pressure(&t6, 6.0).unwrap();
for (i, v) in f.iter().enumerate() {
let want = if i < 3 { 0.0 } else { -1.0 };
assert!((v[2] - want).abs() < 1e-13, "{i}: {v:?}");
}
assert!(pressure(&tri[..2], 1.0).is_err());
}
#[test]
fn pressure_on_a_curved_face_sums_to_the_projected_area() {
// A quadratic face on a quarter cylinder r = 2, z in 0..1, normal outward: the total
// pressure force is −p times the projected areas (2 in x and 2 in y).
let r: f64 = 2.0;
let at = |t: f64, z: f64| [r * t.cos(), r * t.sin(), z];
let h = std::f64::consts::FRAC_PI_2;
// Corners counter-clockwise seen from outside: (0,0), (0,1)... with the normal outward.
let xyz = vec![at(0.0, 0.0), at(h, 0.0), at(h, 1.0), at(0.0, 1.0), at(h / 2.0, 0.0), at(h, 0.5), at(h / 2.0, 1.0), at(0.0, 0.5)];
let w = normal_weights(&xyz).unwrap();
let total = w.iter().fold([0.0; 3], |a, v| [a[0] + v[0], a[1] + v[1], a[2] + v[2]]);
// A quadratic arc interpolates the circle closely; the projected area is exact for the
// interpolated surface (its end points are exact).
assert!((total[0].abs() - 2.0).abs() < 1e-12 && (total[1].abs() - 2.0).abs() < 1e-12 && total[2].abs() < 1e-12, "{total:?}");
assert!(total[0] > 0.0 && total[1] > 0.0, "this ordering points outwards: {total:?}");
}
}
+48
View File
@@ -0,0 +1,48 @@
//! Finite element kernels shared by ModelCraft's structural solvers.
//!
//! Pure functions over element geometry and material constants, with no solver loop and no
//! global state, so the implicit solver (`modelcraft-solver`) and the explicit solver that follows
//! it use the same element technology:
//! - [`quadrature`]: Gauss–Legendre and tetrahedron rules;
//! - [`shape`]: shape functions of tet4, tet10, hex8, hex20 and of their faces;
//! - [`material`]: isotropic and orthotropic elasticity matrices, von Mises stress;
//! - [`element`]: the element table, stiffness (full, reduced, incompatible modes), consistent
//! and lumped mass, body forces, integration-point stresses and their extrapolation to nodes;
//! - [`face`]: consistent nodal forces of pressure on element faces;
//! - [`dense`]: the small dense linear algebra inside an element.
//!
//! Conventions: three translational degrees of freedom per node, ordered node by node; stress
//! and strain 6-vectors in the order xx, yy, zz, xy, xz, yz with engineering shear strains.
#![deny(clippy::unwrap_used, clippy::expect_used, clippy::panic, clippy::unimplemented, clippy::todo, clippy::unreachable)]
#![forbid(unsafe_code)]
// Matrix kernels over fixed small dimensions read as the textbook formulas with index loops.
#![allow(clippy::needless_range_loop)]
pub mod dense;
pub mod element;
pub mod face;
pub mod material;
pub mod quadrature;
pub mod shape;
pub use element::{ELEMENT_TYPES, ElementType, Family, Formulation, PointStress, Solid, element_type};
pub use material::{Elasticity, elasticity, von_mises};
#[derive(Debug, Clone, PartialEq, thiserror::Error)]
pub enum Error {
#[error("invalid input: {0}")]
Invalid(String),
#[error("not supported yet: {0}")]
NotSupported(String),
/// An element's geometry is inverted or collapsed.
#[error("{0}")]
Degenerate(String),
/// A matrix that must be positive definite is not.
#[error("{0}")]
Singular(String),
}
pub type Result<T> = std::result::Result<T, Error>;
#[cfg(test)]
mod tests;
+113
View File
@@ -0,0 +1,113 @@
//! Linear elastic constitutive matrices.
//!
//! Stress and strain are 6-vectors in the order xx, yy, zz, xy, xz, yz, with engineering shear
//! strains (γ = 2ε), so σ = D ε. The order puts the orthotropic shear moduli G₁₂, G₁₃, G₂₃ on
//! the diagonal in the order the model lists them. Material axes are the global axes until the
//! model has material orientations.
//!
//! Orthotropic stiffness is the inverse of the compliance written with engineering constants
//! (R. M. Jones, *Mechanics of Composite Materials*, 2nd ed., Taylor & Francis 1999, §2.4):
//! S₁₁ = 1/E₁, S₁₂ = −ν₁₂/E₁, S₁₃ = −ν₁₃/E₁, S₂₃ = −ν₂₃/E₂ (ν_ji/E_j = ν_ij/E_i), and
//! 1/G on the shear diagonal.
use modelcraft_model::Elastic;
use crate::dense::inverse3;
use crate::{Error, Result};
/// A 6 × 6 elasticity matrix, row-major.
pub type Elasticity = [[f64; 6]; 6];
/// The isotropic elasticity matrix.
pub fn isotropic(young: f64, poisson: f64) -> Result<Elasticity> {
if !(young > 0.0 && young.is_finite() && poisson > -1.0 && poisson < 0.5) {
return Err(Error::Invalid(format!("isotropic constants E = {young}, ν = {poisson} are not a stable material")));
}
let lambda = young * poisson / ((1.0 + poisson) * (1.0 - 2.0 * poisson));
let mu = young / (2.0 * (1.0 + poisson));
let mut d = [[0.0; 6]; 6];
for i in 0..3 {
for j in 0..3 {
d[i][j] = lambda;
}
d[i][i] = lambda + 2.0 * mu;
d[i + 3][i + 3] = mu;
}
Ok(d)
}
/// The orthotropic elasticity matrix from engineering constants.
pub fn orthotropic(young: [f64; 3], poisson: [f64; 3], shear: [f64; 3]) -> Result<Elasticity> {
let [e1, e2, e3] = young;
let [n12, n13, n23] = poisson;
let s = [[1.0 / e1, -n12 / e1, -n13 / e1], [-n12 / e1, 1.0 / e2, -n23 / e2], [-n13 / e1, -n23 / e2, 1.0 / e3]];
let scale = (1.0 / e1) * (1.0 / e2) * (1.0 / e3);
let inverse = inverse3(&s).filter(|(_, det)| *det > 1e-12 * scale);
let Some((normal, _)) = inverse.filter(|_| shear.iter().all(|g| *g > 0.0 && g.is_finite())) else {
return Err(Error::Invalid("the orthotropic constants do not describe a stable material".into()));
};
let mut d = [[0.0; 6]; 6];
for i in 0..3 {
d[i][..3].copy_from_slice(&normal[i]);
}
for (k, g) in shear.iter().enumerate() {
d[3 + k][3 + k] = *g;
}
Ok(d)
}
/// The elasticity matrix of a model material's elastic behaviour.
pub fn elasticity(e: &Elastic) -> Result<Elasticity> {
match *e {
Elastic::Isotropic { young, poisson } => isotropic(young, poisson),
Elastic::EngineeringConstants { young, poisson, shear } => orthotropic(young, poisson, shear),
}
}
/// The von Mises equivalent stress of a stress 6-vector.
pub fn von_mises(s: &[f64; 6]) -> f64 {
let [xx, yy, zz, xy, xz, yz] = *s;
let normal = (xx - yy) * (xx - yy) + (yy - zz) * (yy - zz) + (zz - xx) * (zz - xx);
(0.5 * normal + 3.0 * (xy * xy + xz * xz + yz * yz)).sqrt()
}
/// σ = D ε.
pub fn stress(d: &Elasticity, strain: &[f64; 6]) -> [f64; 6] {
let mut s = [0.0; 6];
for (si, row) in s.iter_mut().zip(d) {
*si = row.iter().zip(strain).map(|(a, b)| a * b).sum();
}
s
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn orthotropic_with_isotropic_constants_is_isotropic() {
let (e, nu) = (210e3, 0.3);
let g = e / (2.0 * (1.0 + nu));
let a = isotropic(e, nu).unwrap();
let b = orthotropic([e; 3], [nu; 3], [g; 3]).unwrap();
for i in 0..6 {
for j in 0..6 {
assert!((a[i][j] - b[i][j]).abs() < 1e-9 * e, "{i} {j}: {} vs {}", a[i][j], b[i][j]);
}
}
assert!(isotropic(1.0, 0.5).is_err());
assert!(orthotropic([1.0; 3], [0.9; 3], [1.0; 3]).is_err());
}
#[test]
fn orthotropic_uniaxial_response() {
// Stress along 1 alone gives strains σ/E1, −ν12 σ/E1, −ν13 σ/E1.
let (young, poisson) = ([140e3, 10e3, 12e3], [0.3, 0.25, 0.4]);
let d = orthotropic(young, poisson, [5e3, 4e3, 3.8e3]).unwrap();
let strain = [1.0 / young[0], -poisson[0] / young[0], -poisson[1] / young[0], 0.0, 0.0, 0.0];
let s = stress(&d, &strain);
assert!((s[0] - 1.0).abs() < 1e-12 && s[1].abs() < 1e-12 && s[2].abs() < 1e-12, "{s:?}");
assert!((von_mises(&[1.0, 0.0, 0.0, 0.0, 0.0, 0.0]) - 1.0).abs() < 1e-15);
assert!((von_mises(&[0.0, 0.0, 0.0, 1.0, 0.0, 0.0]) - 3f64.sqrt()).abs() < 1e-15);
}
}
+161
View File
@@ -0,0 +1,161 @@
//! Numerical integration rules on the reference elements.
//!
//! - Gauss–Legendre rules on [−1, 1] with 1 to 4 points (exact for polynomials of degree
//! 2n − 1), and their tensor products on the reference hexahedron [−1, 1]³.
//! - On the reference tetrahedron {ξ, η, ζ ≥ 0, ξ + η + ζ ≤ 1} (volume 1/6): the centroid rule
//! (degree 1), the symmetric four-point rule (degree 2), and the conical product rule of Stroud
//! (A. H. Stroud, *Approximate Calculation of Multiple Integrals*, Prentice-Hall 1971, §2.7):
//! the collapsed map ξ = u, η = v(1 − u), ζ = w(1 − u)(1 − v) from the unit cube, with
//! Jacobian (1 − u)²(1 − v), integrated by Gauss–Legendre in u, v and w. With n points per
//! direction it is exact for polynomials of degree 2n − 3 on the tetrahedron, with positive
//! weights only.
//! - On the reference triangle {ξ, η ≥ 0, ξ + η ≤ 1}: the same collapsed product in two
//! dimensions (Jacobian 1 − u), exact for degree 2n − 2.
//! - On the reference square [−1, 1]²: tensor Gauss–Legendre.
/// A quadrature point: natural coordinates and weight.
#[derive(Debug, Clone, Copy, PartialEq)]
pub struct Point {
pub xi: [f64; 3],
pub weight: f64,
}
/// Gauss–Legendre abscissae and weights on [−1, 1], `n` in 1..=4 (clamped).
pub fn gauss_legendre(n: usize) -> &'static [(f64, f64)] {
const G1: [(f64, f64); 1] = [(0.0, 2.0)];
const G2: [(f64, f64); 2] = [(-0.577_350_269_189_625_8, 1.0), (0.577_350_269_189_625_8, 1.0)];
const G3: [(f64, f64); 3] = [(-0.774_596_669_241_483_4, 5.0 / 9.0), (0.0, 8.0 / 9.0), (0.774_596_669_241_483_4, 5.0 / 9.0)];
const G4: [(f64, f64); 4] = [
(-0.861_136_311_594_052_6, 0.347_854_845_137_453_9),
(-0.339_981_043_584_856_3, 0.652_145_154_862_546_1),
(0.339_981_043_584_856_3, 0.652_145_154_862_546_1),
(0.861_136_311_594_052_6, 0.347_854_845_137_453_9),
];
match n {
0 | 1 => &G1,
2 => &G2,
3 => &G3,
_ => &G4,
}
}
/// An integration rule on a reference element.
#[derive(Debug, Clone, Copy, PartialEq, Eq, Hash)]
pub enum Rule {
/// n × n × n Gauss–Legendre on the reference hexahedron.
Hex(u8),
/// The tetrahedron's centroid, weight 1/6 (degree 1).
TetCentroid,
/// Four symmetric points on the tetrahedron, weight 1/24 each (degree 2).
Tet4,
/// Stroud's conical product on the tetrahedron, n points per direction.
TetConical(u8),
/// n × n Gauss–Legendre on the reference square (z = 0).
Quad(u8),
/// The collapsed product on the reference triangle, n points per direction (z = 0).
TriConical(u8),
}
impl Rule {
pub fn points(self) -> Vec<Point> {
match self {
Rule::Hex(n) => {
let g = gauss_legendre(usize::from(n));
let mut out = Vec::with_capacity(g.len().pow(3));
// ξ fastest, then η, then ζ: the corner order of the reference hexahedron for 2 × 2 × 2.
for &(z, wz) in g {
for &(y, wy) in g {
for &(x, wx) in g {
out.push(Point { xi: [x, y, z], weight: wx * wy * wz });
}
}
}
out
}
Rule::TetCentroid => vec![Point { xi: [0.25; 3], weight: 1.0 / 6.0 }],
Rule::Tet4 => {
// (5 ∓ √5)/20: the barycentric coordinates of the degree-2 rule.
let a = 0.585_410_196_624_968_5;
let b = 0.138_196_601_125_010_5;
// Point k sits near corner k (barycentric a there, b elsewhere).
[[b, b, b], [a, b, b], [b, a, b], [b, b, a]].into_iter().map(|xi| Point { xi, weight: 1.0 / 24.0 }).collect()
}
Rule::TetConical(n) => {
let g: Vec<(f64, f64)> = gauss_legendre(usize::from(n)).iter().map(|&(x, w)| ((x + 1.0) / 2.0, w / 2.0)).collect();
let mut out = Vec::with_capacity(g.len().pow(3));
for &(u, wu) in &g {
for &(v, wv) in &g {
for &(w, ww) in &g {
let xi = [u, v * (1.0 - u), w * (1.0 - u) * (1.0 - v)];
out.push(Point { xi, weight: wu * wv * ww * (1.0 - u) * (1.0 - u) * (1.0 - v) });
}
}
}
out
}
Rule::Quad(n) => {
let g = gauss_legendre(usize::from(n));
g.iter().flat_map(|&(y, wy)| g.iter().map(move |&(x, wx)| Point { xi: [x, y, 0.0], weight: wx * wy })).collect()
}
Rule::TriConical(n) => {
let g: Vec<(f64, f64)> = gauss_legendre(usize::from(n)).iter().map(|&(x, w)| ((x + 1.0) / 2.0, w / 2.0)).collect();
g.iter()
.flat_map(|&(u, wu)| g.iter().map(move |&(v, wv)| Point { xi: [u, v * (1.0 - u), 0.0], weight: wu * wv * (1.0 - u) }))
.collect()
}
}
}
}
#[cfg(test)]
mod tests {
use super::*;
/// ∫ ξ^a η^b ζ^c over the reference tetrahedron = a! b! c! / (a + b + c + 3)!.
fn tet_monomial(a: u32, b: u32, c: u32) -> f64 {
let f = |n: u32| (1..=n).map(f64::from).product::<f64>();
f(a) * f(b) * f(c) / f(a + b + c + 3)
}
fn integrate(rule: Rule, a: i32, b: i32, c: i32) -> f64 {
rule.points().iter().map(|p| p.weight * p.xi[0].powi(a) * p.xi[1].powi(b) * p.xi[2].powi(c)).sum()
}
#[test]
fn tetrahedron_rules_are_exact_to_their_degree() {
for (rule, degree) in [(Rule::TetCentroid, 1), (Rule::Tet4, 2), (Rule::TetConical(3), 3), (Rule::TetConical(4), 5)] {
for a in 0..=degree {
for b in 0..=degree - a {
for c in 0..=degree - a - b {
let exact = tet_monomial(a, b, c);
let got = integrate(rule, a as i32, b as i32, c as i32);
assert!((got - exact).abs() < 1e-14, "{rule:?} ξ^{a} η^{b} ζ^{c}: {got} vs {exact}");
}
}
}
}
}
#[test]
fn hexahedron_and_face_rules() {
for n in 1..=4u8 {
let d = 2 * i32::from(n) - 1;
for a in 0..=d {
// ∫_{-1}^{1} x^a dx.
let exact_1d = if a % 2 == 1 { 0.0 } else { 2.0 / f64::from(a + 1) };
let got = integrate(Rule::Hex(n), a, 0, 0);
assert!((got - exact_1d * 4.0).abs() < 1e-14, "hex {n} x^{a}");
let got = integrate(Rule::Quad(n), 0, a, 0);
assert!((got - exact_1d * 2.0).abs() < 1e-14, "quad {n} y^{a}");
}
}
// Triangle: ∫ ξ^a η^b = a! b! / (a + b + 2)!.
let f = |n: i32| (1..=n).map(f64::from).product::<f64>();
for a in 0..=4 {
for b in 0..=4 - a {
let got = integrate(Rule::TriConical(3), a, b, 0);
assert!((got - f(a) * f(b) / f(a + b + 2)).abs() < 1e-14, "tri ξ^{a} η^{b}");
}
}
}
}
+192
View File
@@ -0,0 +1,192 @@
//! Shape functions and their derivatives in natural coordinates.
//!
//! Node order is the model's (Abaqus/VTK, [`modelcraft_model::ElementKind`]):
//! - tetrahedra on the reference element with corners (0,0,0), (1,0,0), (0,1,0), (0,0,1) and the
//! volume coordinates L₁ = 1 − ξ − η − ζ, L₂ = ξ, L₃ = η, L₄ = ζ; tet10 mid-side nodes on edges
//! 1-2, 2-3, 3-1, 1-4, 2-4, 3-4 with N = 4 Lₐ L_b, corners N = L(2L − 1);
//! - hexahedra on [−1, 1]³, corners 1–4 at ζ = −1 counter-clockwise from (−1,−1), 5–8 above
//! them; hex20 is the serendipity element (corners
//! N = ⅛(1 + ξξᵢ)(1 + ηηᵢ)(1 + ζζᵢ)(ξξᵢ + ηηᵢ + ζζᵢ − 2), a mid-side node with ξᵢ = 0
//! N = ¼(1 − ξ²)(1 + ηηᵢ)(1 + ζζᵢ), and likewise), mid-side nodes 9–12 on the bottom edges,
//! 13–16 on the top edges, 17–20 on the vertical edges (mid-side positions come from
//! [`modelcraft_model::ElementKind::edges`], the one place the node order is written down).
//!
//! The functions are the textbook ones (O. C. Zienkiewicz, R. L. Taylor, J. Z. Zhu, *The Finite
//! Element Method: Its Basis and Fundamentals*, 7th ed., Butterworth-Heinemann 2013, ch. 6;
//! T. J. R. Hughes, *The Finite Element Method*, Dover 2000, ch. 3).
use modelcraft_model::ElementKind;
/// Most nodes an element in this crate has (hex20).
pub const MAX_NODES: usize = 20;
/// Shape function values and natural derivatives at one point.
#[derive(Debug, Clone, Copy)]
pub struct Shape {
pub count: usize,
pub n: [f64; MAX_NODES],
/// ∂Nᵢ/∂ξ, ∂Nᵢ/∂η, ∂Nᵢ/∂ζ.
pub dn: [[f64; 3]; MAX_NODES],
}
impl Shape {
fn new(count: usize) -> Shape {
Shape { count, n: [0.0; MAX_NODES], dn: [[0.0; 3]; MAX_NODES] }
}
pub fn values(&self) -> &[f64] {
self.n.get(..self.count).unwrap_or_default()
}
pub fn derivatives(&self) -> &[[f64; 3]] {
self.dn.get(..self.count).unwrap_or_default()
}
}
/// Natural coordinates of the hexahedron's corners.
pub const HEX_CORNERS: [[f64; 3]; 8] =
[[-1., -1., -1.], [1., -1., -1.], [1., 1., -1.], [-1., 1., -1.], [-1., -1., 1.], [1., -1., 1.], [1., 1., 1.], [-1., 1., 1.]];
/// Natural coordinates of the tetrahedron's corners.
pub const TET_CORNERS: [[f64; 3]; 4] = [[0., 0., 0.], [1., 0., 0.], [0., 1., 0.], [0., 0., 1.]];
/// Four-node tetrahedron.
pub fn tet4(xi: [f64; 3]) -> Shape {
let mut s = Shape::new(4);
s.n[0] = 1.0 - xi[0] - xi[1] - xi[2];
s.n[1] = xi[0];
s.n[2] = xi[1];
s.n[3] = xi[2];
s.dn[0] = [-1.0, -1.0, -1.0];
s.dn[1] = [1.0, 0.0, 0.0];
s.dn[2] = [0.0, 1.0, 0.0];
s.dn[3] = [0.0, 0.0, 1.0];
s
}
/// Ten-node tetrahedron.
pub fn tet10(xi: [f64; 3]) -> Shape {
let lin = tet4(xi);
let l = [lin.n[0], lin.n[1], lin.n[2], lin.n[3]];
let dl = [lin.dn[0], lin.dn[1], lin.dn[2], lin.dn[3]];
let mut s = Shape::new(10);
for i in 0..4 {
s.n[i] = l[i] * (2.0 * l[i] - 1.0);
s.dn[i] = dl[i].map(|d| (4.0 * l[i] - 1.0) * d);
}
// Mid-side nodes on the model's tet10 edges.
for edge in ElementKind::Tet10.edges() {
if let [a, b, m] = **edge {
s.n[m] = 4.0 * l[a] * l[b];
s.dn[m] = [0, 1, 2].map(|c| 4.0 * (dl[a][c] * l[b] + l[a] * dl[b][c]));
}
}
s
}
/// Eight-node hexahedron (trilinear).
pub fn hex8(xi: [f64; 3]) -> Shape {
let mut s = Shape::new(8);
for (i, c) in HEX_CORNERS.iter().enumerate() {
let f = [0, 1, 2].map(|k| 1.0 + xi[k] * c[k]);
s.n[i] = f[0] * f[1] * f[2] / 8.0;
s.dn[i] = [c[0] * f[1] * f[2] / 8.0, c[1] * f[0] * f[2] / 8.0, c[2] * f[0] * f[1] / 8.0];
}
s
}
/// Twenty-node serendipity hexahedron.
pub fn hex20(xi: [f64; 3]) -> Shape {
let mut s = Shape::new(20);
let [x, y, z] = xi;
for (i, c) in HEX_CORNERS.iter().enumerate() {
let f = [0, 1, 2].map(|k| 1.0 + xi[k] * c[k]);
let g = x * c[0] + y * c[1] + z * c[2] - 2.0;
s.n[i] = f[0] * f[1] * f[2] * g / 8.0;
// ∂/∂ξ_k: c_k f_l f_m g / 8 + f_0 f_1 f_2 c_k / 8.
s.dn[i] = [c[0] * f[1] * f[2] * (g + f[0]) / 8.0, c[1] * f[0] * f[2] * (g + f[1]) / 8.0, c[2] * f[0] * f[1] * (g + f[2]) / 8.0];
}
// Mid-side nodes on the model's hex20 edges, at the midpoints of their corners.
for edge in ElementKind::Hex20.edges() {
let [a, b, i] = **edge else { continue };
let c = [0, 1, 2].map(|k| (HEX_CORNERS[a][k] + HEX_CORNERS[b][k]) / 2.0);
// The direction along the edge has cᵢ = 0: N = ¼(1 − t²)(1 + a aᵢ)(1 + b bᵢ).
let along = if c[0] == 0.0 {
0
} else if c[1] == 0.0 {
1
} else {
2
};
let (p, q) = ((along + 1) % 3, (along + 2) % 3);
let t = xi[along];
let fp = 1.0 + xi[p] * c[p];
let fq = 1.0 + xi[q] * c[q];
s.n[i] = (1.0 - t * t) * fp * fq / 4.0;
let mut d = [0.0; 3];
d[along] = -2.0 * t * fp * fq / 4.0;
d[p] = (1.0 - t * t) * c[p] * fq / 4.0;
d[q] = (1.0 - t * t) * fp * c[q] / 4.0;
s.dn[i] = d;
}
s
}
#[cfg(test)]
mod tests {
use super::*;
fn nodes_of(kind: &str) -> Vec<[f64; 3]> {
match kind {
"tet4" => TET_CORNERS.to_vec(),
"tet10" => {
let mut v = TET_CORNERS.to_vec();
for e in ElementKind::Tet10.edges() {
v.push([0, 1, 2].map(|k| (TET_CORNERS[e[0]][k] + TET_CORNERS[e[1]][k]) / 2.0));
}
v
}
"hex8" => HEX_CORNERS.to_vec(),
_ => {
let mut v = HEX_CORNERS.to_vec();
for e in ElementKind::Hex20.edges() {
v.push([0, 1, 2].map(|k| (HEX_CORNERS[e[0]][k] + HEX_CORNERS[e[1]][k]) / 2.0));
}
v
}
}
}
#[test]
fn kronecker_delta_partition_of_unity_and_derivatives() {
let kinds: [(&str, fn([f64; 3]) -> Shape); 4] = [("tet4", tet4), ("tet10", tet10), ("hex8", hex8), ("hex20", hex20)];
for (name, f) in kinds {
let nodes = nodes_of(name);
for (i, p) in nodes.iter().enumerate() {
let s = f(*p);
for (j, v) in s.values().iter().enumerate() {
assert!((v - if i == j { 1.0 } else { 0.0 }).abs() < 1e-14, "{name} N{j} at node {i}: {v}");
}
}
// At an arbitrary point: ΣN = 1, ΣdN = 0, Σ N x = x (linear completeness), and the
// derivatives match central differences.
let p = [0.21, 0.17, 0.33];
let s = f(p);
assert!((s.values().iter().sum::<f64>() - 1.0).abs() < 1e-14);
for k in 0..3 {
assert!(s.derivatives().iter().map(|d| d[k]).sum::<f64>().abs() < 1e-13);
let x: f64 = s.values().iter().zip(&nodes).map(|(n, x)| n * x[k]).sum();
assert!((x - p[k]).abs() < 1e-14, "{name}");
let h = 1e-6;
let (mut a, mut b) = (p, p);
a[k] += h;
b[k] -= h;
let (sa, sb) = (f(a), f(b));
for j in 0..s.count {
let fd = (sa.n[j] - sb.n[j]) / (2.0 * h);
assert!((fd - s.dn[j][k]).abs() < 1e-8, "{name} dN{j}/dξ{k}: {fd} vs {}", s.dn[j][k]);
}
}
}
}
}
+206
View File
@@ -0,0 +1,206 @@
//! Element-level checks: rigid-body modes, constant-strain reproduction (the single-element form
//! of the patch test), mass and load totals, extrapolation.
use modelcraft_model::ElementKind;
use crate::dense::{Cholesky, Matrix};
use crate::element::{Formulation, Solid};
use crate::material::{isotropic, orthotropic, stress};
/// A distorted but valid element of each kind, mid-side nodes off the straight edges for the
/// quadratic kinds when `curved`.
fn distorted(kind: ElementKind, curved: bool) -> Vec<[f64; 3]> {
let corners: Vec<[f64; 3]> = match kind {
ElementKind::Tet4 | ElementKind::Tet10 => vec![[0.1, -0.05, 0.0], [1.2, 0.1, 0.05], [0.2, 0.9, -0.1], [0.05, 0.15, 1.1]],
_ => vec![
[0.0, 0.0, 0.0],
[2.1, 0.1, -0.1],
[2.3, 1.2, 0.05],
[-0.1, 0.9, 0.1],
[0.1, -0.1, 0.8],
[2.0, 0.05, 1.1],
[2.2, 1.1, 0.9],
[0.05, 1.05, 1.2],
],
};
let mut xyz = corners.clone();
for (i, e) in kind.edges().iter().enumerate() {
if let [a, b, _] = **e {
let bump = if curved { 0.03 * ((i % 3) as f64 - 1.0) } else { 0.0 };
xyz.push([0, 1, 2].map(|k| (corners[a][k] + corners[b][k]) / 2.0 + bump));
}
}
xyz
}
const CASES: [(ElementKind, Formulation); 6] = [
(ElementKind::Tet4, Formulation::Full),
(ElementKind::Tet10, Formulation::Full),
(ElementKind::Hex8, Formulation::Full),
(ElementKind::Hex8, Formulation::IncompatibleModes),
(ElementKind::Hex20, Formulation::Full),
(ElementKind::Hex20, Formulation::Reduced),
];
fn rigid_modes(xyz: &[[f64; 3]]) -> Vec<Vec<f64>> {
let mut modes = Vec::new();
for k in 0..3 {
modes.push(xyz.iter().flat_map(|_| [0, 1, 2].map(|c| if c == k { 1.0 } else { 0.0 })).collect());
}
for axis in 0..3 {
// ω × x for ω along `axis`.
let w = [0, 1, 2].map(|c| if c == axis { 1.0 } else { 0.0 });
modes.push(xyz.iter().flat_map(|x| [w[1] * x[2] - w[2] * x[1], w[2] * x[0] - w[0] * x[2], w[0] * x[1] - w[1] * x[0]]).collect());
}
modes
}
#[test]
fn stiffness_is_symmetric_with_exactly_six_rigid_body_modes() {
let d = isotropic(1000.0, 0.3).unwrap();
for (kind, f) in CASES {
let xyz = distorted(kind, true);
let k = Solid::new(kind, &xyz, f).unwrap().stiffness(&d).unwrap();
let scale = k.data.iter().fold(0.0f64, |m, v| m.max(v.abs()));
for i in 0..k.n {
for j in 0..k.n {
assert_eq!(k.get(i, j), k.get(j, i), "{kind:?} {f:?} symmetric");
}
}
for m in rigid_modes(&xyz) {
let r = k.mul_vec(&m);
assert!(r.iter().all(|v| v.abs() < 1e-10 * scale), "{kind:?} {f:?}: rigid motion strains the element");
}
// Holding six degrees of freedom (node 1 fully, node 2 in y and z, node 3 in z) leaves a
// positive definite matrix: no other zero-energy mode. Reduced hex20 has spurious modes
// on a single element, so it is skipped.
if f != Formulation::Reduced {
let mut held = k.clone();
for dof in [0, 1, 2, 4, 5, 8] {
held.add(dof, dof, 1e3 * scale);
}
assert!(Cholesky::new(&held).is_ok(), "{kind:?} {f:?} has a spurious zero-energy mode");
}
}
}
#[test]
fn constant_strain_is_reproduced_exactly() {
// u = A x for a general A: every integration point sees ε(A), the stiffness's internal
// forces balance (K u is the boundary load of a uniform stress), and the incompatible modes
// stay idle.
let a = [[1e-3, 2e-4, -3e-4], [5e-4, -2e-3, 1e-4], [-1e-4, 3e-4, 7e-4]];
let strain = [a[0][0], a[1][1], a[2][2], a[0][1] + a[1][0], a[0][2] + a[2][0], a[1][2] + a[2][1]];
for d in [isotropic(210e3, 0.3).unwrap(), orthotropic([140e3, 10e3, 12e3], [0.3, 0.25, 0.4], [5e3, 4e3, 3.8e3]).unwrap()] {
let want = stress(&d, &strain);
for (kind, f) in CASES {
// Curved mid-sides keep the field in the isoparametric span only for straight edges.
let xyz = distorted(kind, false);
let u: Vec<[f64; 3]> = xyz.iter().map(|x| [0, 1, 2].map(|i| (0..3).map(|j| a[i][j] * x[j]).sum())).collect();
let e = Solid::new(kind, &xyz, f).unwrap();
for p in e.stresses(&d, &u).unwrap() {
for k in 0..6 {
assert!((p.strain[k] - strain[k]).abs() < 1e-14, "{kind:?} {f:?} strain {k}");
assert!((p.stress[k] - want[k]).abs() < 1e-9 * want[0].abs().max(1.0), "{kind:?} {f:?} stress {k}");
}
}
let nodal = e.extrapolate(&e.stresses(&d, &u).unwrap().iter().map(|p| p.stress).collect::<Vec<_>>()).unwrap();
assert_eq!(nodal.len(), xyz.len());
assert!(nodal.iter().all(|s| (0..6).all(|k| (s[k] - want[k]).abs() < 1e-9 * want[0].abs())), "{kind:?} {f:?}");
}
}
}
#[test]
fn mass_volume_and_body_force_totals() {
let rho = 7.85e-9;
for (kind, f) in CASES {
let xyz = distorted(kind, true);
let e = Solid::new(kind, &xyz, f).unwrap();
let v = e.volume().unwrap();
assert!(v > 0.0);
let m = e.mass(rho).unwrap();
let total: f64 = m.data.iter().sum();
assert!((total - rho * v).abs() < 1e-12 * rho * v, "{kind:?}: {total} vs {}", rho * v);
let lumped = e.lumped_mass(rho).unwrap();
assert!(lumped.iter().all(|x| *x > 0.0), "{kind:?}: lumped masses are positive");
assert!((lumped.iter().sum::<f64>() - rho * v).abs() < 1e-12 * rho * v);
let b = e.body_force([0.0, 0.0, -9.81]).unwrap();
assert!((b.iter().map(|f| f[2]).sum::<f64>() + 9.81 * v).abs() < 1e-12 * v);
}
// A tetrahedron's volume is a sixth of its edge triple product.
let xyz = distorted(ElementKind::Tet4, false);
let e = |i: usize| [0, 1, 2].map(|k| xyz[i][k] - xyz[0][k]);
let (a, b, c) = (e(1), e(2), e(3));
let exact = (a[0] * (b[1] * c[2] - b[2] * c[1]) - a[1] * (b[0] * c[2] - b[2] * c[0]) + a[2] * (b[0] * c[1] - b[1] * c[0])) / 6.0;
let v = Solid::new(ElementKind::Tet4, &xyz, Formulation::Full).unwrap().volume().unwrap();
assert!((v - exact).abs() < 1e-15);
}
#[test]
fn extrapolation_reproduces_linear_fields_on_affine_elements() {
// Values linear in x at the integration points come back exactly at the nodes (tet4 has
// one point and gives the mean).
let f = |x: [f64; 3]| 1.0 + 2.0 * x[0] - 0.5 * x[1] + 3.0 * x[2];
let affine = |kind: ElementKind| -> Vec<[f64; 3]> {
let mut xyz: Vec<[f64; 3]> = match kind {
ElementKind::Tet10 => vec![[0., 0., 0.], [1., 0., 0.], [0., 1., 0.], [0., 0., 1.]],
_ => vec![[0., 0., 0.], [2., 0., 0.], [2.5, 1., 0.], [0.5, 1., 0.], [0., 0., 1.], [2., 0., 1.], [2.5, 1., 1.], [0.5, 1., 1.]],
};
let c = xyz.clone();
for e in kind.edges() {
if let [a, b, _] = **e {
xyz.push([0, 1, 2].map(|k| (c[a][k] + c[b][k]) / 2.0));
}
}
xyz
};
for (kind, form) in CASES.into_iter().filter(|(k, _)| *k != ElementKind::Tet4) {
let xyz = affine(kind);
let e = Solid::new(kind, &xyz, form).unwrap();
let values: Vec<[f64; 6]> = e.integration_points().iter().map(|p| [f(e.position(p.xi)); 6]).collect();
let nodal = e.extrapolate(&values).unwrap();
for (x, v) in xyz.iter().zip(&nodal) {
assert!((v[0] - f(*x)).abs() < 1e-12, "{kind:?} {form:?} at {x:?}: {} vs {}", v[0], f(*x));
}
}
}
#[test]
fn bad_input_is_an_error() {
let xyz = distorted(ElementKind::Hex8, false);
assert!(Solid::new(ElementKind::Hex8, &xyz[..7], Formulation::Full).is_err());
assert!(Solid::new(ElementKind::Hex8, &xyz, Formulation::Reduced).is_err());
assert!(Solid::new(ElementKind::Tet4, &xyz[..4], Formulation::IncompatibleModes).is_err());
assert!(Solid::new(ElementKind::Wedge6, &xyz[..6], Formulation::Full).is_err());
let mut nan = xyz.clone();
nan[3][1] = f64::NAN;
assert!(Solid::new(ElementKind::Hex8, &nan, Formulation::Full).is_err());
// An inverted element (top and bottom swapped) and a flat one.
let mut inverted = xyz.clone();
inverted.rotate_left(4);
let d = isotropic(1.0, 0.3).unwrap();
assert!(Solid::new(ElementKind::Hex8, &inverted, Formulation::Full).unwrap().stiffness(&d).is_err());
let flat: Vec<[f64; 3]> = xyz.iter().map(|p| [p[0], p[1], 0.0]).collect();
assert!(Solid::new(ElementKind::Hex8, &flat, Formulation::IncompatibleModes).unwrap().stiffness(&d).is_err());
let e = Solid::new(ElementKind::Hex8, &xyz, Formulation::Full).unwrap();
assert!(e.stresses(&d, &[[0.0; 3]; 3]).is_err());
assert!(e.extrapolate(&[[0.0; 6]; 3]).is_err());
let _ = Matrix::zeros(0).mul_vec(&[]);
}
#[test]
fn section_formulations() {
use modelcraft_model::{Formulation as F, Integration};
let full = F::default();
let reduced = F { integration: Integration::Reduced, ..F::default() };
let im = F { incompatible_modes: true, ..F::default() };
let hybrid = F { hybrid: true, ..F::default() };
assert_eq!(Formulation::from_section(ElementKind::Hex8, &full), Ok(Formulation::Full));
assert_eq!(Formulation::from_section(ElementKind::Hex8, &im), Ok(Formulation::IncompatibleModes));
assert_eq!(Formulation::from_section(ElementKind::Hex20, &reduced), Ok(Formulation::Reduced));
assert!(Formulation::from_section(ElementKind::Hex8, &reduced).unwrap_err().to_string().contains("not supported yet"));
assert!(Formulation::from_section(ElementKind::Tet10, &im).is_err());
assert!(Formulation::from_section(ElementKind::Tet4, &hybrid).is_err());
assert!(Formulation::from_section(ElementKind::Quad4, &full).is_err());
}
+51 -20
View File
@@ -95,6 +95,48 @@ fn rule(corners: usize) -> Vec<(f64, f64, f64)> {
}
}
/// Visit the quadrature points of a face (node coordinates in the face's node order): the shape
/// function values and the weighted normal (∂x/∂ξ × ∂x/∂η) w, whose length is the point's share of
/// the area and whose direction is the face's right-hand normal.
fn integrate_face(xyz: &[[f64; 3]], mut visit: impl FnMut(&[f64], [f64; 3])) -> Result<()> {
if xyz.iter().flatten().any(|c| !c.is_finite()) {
return Err(Error::Invalid("face coordinates must be finite".into()));
}
let (corners, shape): (usize, fn(usize, f64, f64) -> Shape) = match xyz.len() {
3 | 6 => (3, triangle),
4 | 8 => (4, quadrilateral),
n => return Err(Error::Invalid(format!("a face has 3, 4, 6 or 8 nodes, not {n}"))),
};
for (xi, eta, w) in rule(corners) {
let s = shape(xyz.len(), xi, eta);
let mut tx = [0.0; 3];
let mut te = [0.0; 3];
for ((p, dx), de) in xyz.iter().zip(&s.dxi).zip(&s.deta) {
for k in 0..3 {
tx[k] += dx * p[k];
te[k] += de * p[k];
}
}
let c = [tx[1] * te[2] - tx[2] * te[1], tx[2] * te[0] - tx[0] * te[2], tx[0] * te[1] - tx[1] * te[0]];
visit(&s.n, c.map(|v| v * w));
}
Ok(())
}
/// ∫ Nᵢ n dA for every node of a face: the consistent nodal forces of a unit pressure pulling
/// along the face's right-hand (outward, for solids) normal.
pub fn face_normal_weights(xyz: &[[f64; 3]]) -> Result<Vec<[f64; 3]>> {
let mut out = vec![[0.0; 3]; xyz.len()];
integrate_face(xyz, |n, nda| {
for (o, ni) in out.iter_mut().zip(n) {
for k in 0..3 {
o[k] += ni * nda[k];
}
}
})?;
Ok(out)
}
impl Model {
/// The nodal weights `∫ N_i dA` of a set of element faces, summed per node. Their sum is the
/// faces' area.
@@ -104,27 +146,16 @@ impl Model {
let labels = self.face_nodes(f).ok_or_else(|| Error::NotFound(format!("element {} face {}", f.element, f.face)))?;
let xyz: Vec<[f64; 3]> =
labels.iter().map(|n| self.node(*n).map(|p| p.xyz).ok_or_else(|| Error::NotFound(format!("node {n}")))).collect::<Result<_>>()?;
let (corners, shape): (usize, fn(usize, f64, f64) -> Shape) = match labels.len() {
3 | 6 => (3, triangle),
4 | 8 => (4, quadrilateral),
n => return Err(Error::Invalid(format!("element {} face {} has {n} nodes, not a surface face", f.element, f.face))),
};
for (xi, eta, w) in rule(corners) {
let s = shape(labels.len(), xi, eta);
let mut tx = [0.0; 3];
let mut te = [0.0; 3];
for ((p, dx), de) in xyz.iter().zip(&s.dxi).zip(&s.deta) {
for k in 0..3 {
tx[k] += dx * p[k];
te[k] += de * p[k];
}
integrate_face(&xyz, |n, nda| {
let da = (nda[0] * nda[0] + nda[1] * nda[1] + nda[2] * nda[2]).sqrt();
for (label, ni) in labels.iter().zip(n) {
*out.entry(*label).or_default() += ni * da;
}
let c = [tx[1] * te[2] - tx[2] * te[1], tx[2] * te[0] - tx[0] * te[2], tx[0] * te[1] - tx[1] * te[0]];
let da = (c[0] * c[0] + c[1] * c[1] + c[2] * c[2]).sqrt() * w;
for (label, n) in labels.iter().zip(&s.n) {
*out.entry(*label).or_default() += n * da;
}
}
})
.map_err(|e| match e {
Error::Invalid(m) => Error::Invalid(format!("element {} face {}: {m}", f.element, f.face)),
e => e,
})?;
}
Ok(out)
}
+15
View File
@@ -0,0 +1,15 @@
[package]
name = "modelcraft-solver"
description = "ModelCraft's implicit solver: assembly, boundary conditions, sparse Cholesky, linear static and frequency analysis"
version.workspace = true
edition.workspace = true
license.workspace = true
[lints]
workspace = true
[dependencies]
modelcraft-model = { workspace = true }
modelcraft-fem = { workspace = true }
thiserror = { workspace = true }
serde = { workspace = true }
+431
View File
@@ -0,0 +1,431 @@
//! Linear static and frequency analysis of a model's step, and their results.
use modelcraft_fem::element::{Extrapolation, extrapolation};
use modelcraft_fem::quadrature::Rule;
use modelcraft_fem::{PointStress, von_mises};
use modelcraft_model::{ElementKind, Model, Procedure, Resolved, Step};
use serde::Serialize;
use crate::cholesky::{Factor, FactorError, UpperColumns};
use crate::eigen::{Operator, Wanted, lanczos};
use crate::ordering::nested_dissection;
use crate::sparse::{Csr, NodeGraph, add_block, add_diagonal, add_scalar};
use crate::system::{Mesh, equations, loads, prescribed};
use crate::{Error, Limits, Result};
/// Size and effort of a solution.
#[derive(Debug, Clone, Default, PartialEq, Serialize)]
pub struct Stats {
/// Degrees of freedom of the mesh (3 per node).
pub dofs: usize,
/// Free degrees of freedom solved for.
pub equations: usize,
/// Entries in the Cholesky factor.
pub factor_entries: usize,
/// Lanczos vectors used (frequency analysis).
pub lanczos_vectors: usize,
}
/// Stresses of one element.
#[derive(Debug, Clone, PartialEq)]
pub struct ElementStress {
pub label: u32,
pub kind: ElementKind,
/// At the integration points.
pub points: Vec<PointStress>,
/// Extrapolated to the element's nodes, in its node order.
pub nodal: Vec<[f64; 6]>,
}
/// The result of a static step.
#[derive(Debug, Clone, PartialEq)]
pub struct StaticResult {
pub step: String,
/// Node labels with degrees of freedom, sorted; the per-node vectors follow this order.
pub nodes: Vec<u32>,
pub displacement: Vec<[f64; 3]>,
/// Reaction forces (zero where nothing is prescribed).
pub reaction: Vec<[f64; 3]>,
/// Stress averaged at the nodes over the elements that share them (xx, yy, zz, xy, xz, yz).
pub stress: Vec<[f64; 6]>,
/// Von Mises stress of the averaged nodal stress.
pub von_mises: Vec<f64>,
pub elements: Vec<ElementStress>,
/// Sum of the applied loads and of the reactions.
pub applied_total: [f64; 3],
pub reaction_total: [f64; 3],
pub stats: Stats,
pub warnings: Vec<String>,
}
/// One natural mode.
#[derive(Debug, Clone, PartialEq)]
pub struct Mode {
/// λ = ω², in (rad per time unit)².
pub eigenvalue: f64,
/// Cycles per time unit (0 for a rigid-body mode).
pub frequency: f64,
/// Mass-normalized (φᵀ M φ = 1), per node in [`FrequencyResult::nodes`] order.
pub shape: Vec<[f64; 3]>,
/// Participation factors Γ = φᵀ M r for unit translations along X, Y, Z.
pub participation: [f64; 3],
/// Effective mass Γ² along X, Y, Z.
pub effective_mass: [f64; 3],
}
/// The result of a frequency step.
#[derive(Debug, Clone, PartialEq)]
pub struct FrequencyResult {
pub step: String,
pub nodes: Vec<u32>,
pub modes: Vec<Mode>,
/// Mass of the model.
pub total_mass: f64,
pub stats: Stats,
pub warnings: Vec<String>,
}
/// Mass matrix choice for a frequency analysis.
#[derive(Debug, Clone, Copy, Default, PartialEq, Eq, Serialize, serde::Deserialize)]
#[serde(rename_all = "snake_case")]
pub enum MassKind {
#[default]
Consistent,
Lumped,
}
/// Options of a frequency analysis.
#[derive(Debug, Clone, Copy, Default)]
pub struct FrequencyOptions {
pub mass: MassKind,
/// The spectral shift σ (eigenvalue units); by default 0 for a supported structure and a
/// small negative value for a free one.
pub shift: Option<f64>,
}
/// The step named `name`, or the only step of the procedure when no name is given; it must be
/// of that procedure.
fn select_step<'m>(model: &'m Model, name: Option<&str>, wanted: fn(&Procedure) -> bool, what: &str) -> Result<&'m Step> {
let step = match name {
Some(n) => model.step(n).ok_or_else(|| Error::Invalid(format!("step `{n}` does not exist")))?,
None => {
let matching: Vec<&Step> = model.steps().iter().filter(|s| wanted(&s.procedure)).collect();
match matching.as_slice() {
[one] => *one,
[] => return Err(Error::Invalid(format!("the model has no {what} step"))),
many => {
let names: Vec<&str> = many.iter().map(|s| s.name.as_str()).collect();
return Err(Error::Invalid(format!("name the step: the model has {what} steps {}", names.join(", "))));
}
}
}
};
if !wanted(&step.procedure) {
return Err(Error::Invalid(format!("step `{}` is a {} step, not a {what} one", step.name, step.procedure.name())));
}
Ok(step)
}
/// The assembled matrices and the model's mass.
struct Assembled {
k: Csr,
m: Option<Csr>,
}
/// Assemble the stiffness (and the mass when `mass` is set) on the mesh's node graph.
fn assemble(mesh: &Mesh, graph: &NodeGraph, mass: Option<MassKind>) -> Result<Assembled> {
let mut k = graph.zero_matrix();
let mut m = mass.map(|_| graph.zero_matrix());
for e in &mesh.elements {
let solid = e.solid()?;
let at = |err| Error::element(e.label, err);
add_block(&mut k, &e.nodes, &solid.stiffness(&e.d).map_err(at)?.data)?;
if let (Some(mm), Some(kind)) = (m.as_mut(), mass) {
let rho = e.density.ok_or_else(|| Error::Invalid(format!("element {} has no density", e.label)))?;
match kind {
MassKind::Consistent => add_scalar(mm, &e.nodes, &solid.mass(rho).map_err(at)?.data)?,
MassKind::Lumped => add_diagonal(mm, &e.nodes, &solid.lumped_mass(rho).map_err(at)?)?,
}
}
}
Ok(Assembled { k, m })
}
/// Factor a free-dof matrix; a singular pivot is reported as the free-dof column it hit.
fn factor_raw(a: &Csr, limits: &Limits) -> std::result::Result<Factor, FactorError> {
Factor::new(&UpperColumns::from_symmetric(a), limits.max_factor_entries)
}
/// A factorization failure in the user's terms: the node and direction of a singular pivot.
fn factor_error(e: FactorError, mesh: &Mesh, map: &[Option<usize>]) -> Error {
match e {
FactorError::TooLarge { entries, limit } => {
Error::Limit(format!("the factorization needs {entries} entries; the limit is {limit} (refine less or raise the limit)"))
}
FactorError::NotPositiveDefinite { column } => {
let dof = map.iter().position(|m| *m == Some(column)).unwrap_or(0);
let label = mesh.labels.get(dof / 3).copied().unwrap_or(0);
let axis = ["X", "Y", "Z"].get(dof % 3).copied().unwrap_or("?");
Error::Singular(format!(
"the stiffness is singular at node {label} in {axis}: the model can move without straining (missing or insufficient boundary conditions, or a part not connected to the rest)"
))
}
}
}
/// Spread a free-equation vector over every degree of freedom (`base` holds the prescribed
/// values) and group it per node.
fn per_node(x: &[f64], map: &[Option<usize>], base: Vec<f64>) -> Vec<[f64; 3]> {
let mut full = base;
for (dof, m) in map.iter().enumerate() {
if let (Some(eq), Some(v)) = (m, full.get_mut(dof)) {
*v = x.get(*eq).copied().unwrap_or(0.0);
}
}
full.as_chunks::<3>().0.to_vec()
}
/// Solve a linear static step: the step named `step`, or the model's only static step.
pub fn solve_static(model: &Model, step: Option<&str>, limits: &Limits) -> Result<StaticResult> {
let resolved = model.resolve()?;
let step = select_step(model, step, |p| matches!(p, Procedure::Static {}), "static")?;
let mesh = Mesh::new(model, &resolved, limits.max_dofs)?;
let fixed = prescribed(model, &resolved, &mesh, step, true)?;
let f = loads(model, &resolved, &mesh, step)?;
let graph = NodeGraph::new(mesh.labels.len(), mesh.elements.iter().map(|e| e.nodes.as_slice()));
let k = assemble(&mesh, &graph, None)?.k;
let (map, neq) = equations(&nested_dissection(&mesh.xyz, &graph.adjacency), &fixed);
if neq == 0 {
return Err(Error::Invalid("every degree of freedom is prescribed; there is nothing to solve".into()));
}
let chol = factor_raw(&k.restrict(&map, neq), limits).map_err(|e| factor_error(e, &mesh, &map))?;
// Right-hand side: f_free − K_fp u_p (K u_p only when something moves).
let up: Vec<f64> = fixed.iter().map(|v| v.unwrap_or(0.0)).collect();
let mut kup = vec![0.0; mesh.dofs()];
if up.iter().any(|v| *v != 0.0) {
k.mul(&up, &mut kup);
}
let mut rhs = vec![0.0; neq];
for (dof, m) in map.iter().enumerate() {
if let (Some(eq), Some(fv), Some(kv)) = (m, f.get(dof), kup.get(dof))
&& let Some(r) = rhs.get_mut(*eq)
{
*r = fv - kv;
}
}
chol.solve(&mut rhs)?;
let displacement = per_node(&rhs, &map, up);
if displacement.iter().flatten().any(|x| !x.is_finite()) {
return Err(Error::Singular("the solution is not finite; the model is ill-conditioned".into()));
}
// Reactions R = K u − f at the prescribed degrees of freedom (only their rows of K).
let mut reaction = vec![[0.0; 3]; mesh.labels.len()];
let (mut applied_total, mut reaction_total) = ([0.0; 3], [0.0; 3]);
for (dof, fv) in f.iter().enumerate() {
let (node, c) = (dof / 3, dof % 3);
applied_total[c] += fv;
if fixed.get(dof).is_some_and(Option::is_some) {
let (cols, vals) = k.row(dof);
let ku: f64 = cols.iter().zip(vals).map(|(j, v)| v * displacement.get(j / 3).map_or(0.0, |u| u[j % 3])).sum();
if let Some(rn) = reaction.get_mut(node) {
rn[c] = ku - fv;
}
reaction_total[c] += ku - fv;
}
}
// Stresses: one extrapolation per element type and rule.
let mut extrapolations: Vec<(ElementKind, Rule, Extrapolation)> = Vec::new();
let mut elements = Vec::with_capacity(mesh.elements.len());
let mut sum = vec![[0.0; 6]; mesh.labels.len()];
let mut count = vec![0u32; mesh.labels.len()];
for e in &mesh.elements {
let solid = e.solid()?;
let at = |err| Error::element(e.label, err);
let ue: Vec<[f64; 3]> = e.nodes.iter().map(|n| displacement.get(*n).copied().unwrap_or_default()).collect();
let points = solid.stresses(&e.d, &ue).map_err(at)?;
let values: Vec<[f64; 6]> = points.iter().map(|p| p.stress).collect();
let rule = solid.rule();
let cached = extrapolations.iter().position(|(k, r, _)| *k == e.kind && *r == rule);
let index = match cached {
Some(i) => i,
None => {
extrapolations.push((e.kind, rule, extrapolation(solid.ty, rule).map_err(at)?));
extrapolations.len() - 1
}
};
let nodal = extrapolations.get(index).map(|(_, _, x)| x.apply(&values)).unwrap_or_default();
for (n, s) in e.nodes.iter().zip(&nodal) {
if let (Some(acc), Some(c)) = (sum.get_mut(*n), count.get_mut(*n)) {
for k in 0..6 {
acc[k] += s[k];
}
*c += 1;
}
}
elements.push(ElementStress { label: e.label, kind: e.kind, points, nodal });
}
let stress: Vec<[f64; 6]> = sum.iter().zip(&count).map(|(s, c)| s.map(|v| if *c > 0 { v / f64::from(*c) } else { 0.0 })).collect();
let von_mises = stress.iter().map(von_mises).collect();
let mut warnings: Vec<String> = resolved.warnings.iter().map(ToString::to_string).collect();
let scale = applied_total.iter().chain(&reaction_total).fold(0.0f64, |m, v| m.max(v.abs()));
let imbalance = (0..3).map(|c| (applied_total[c] + reaction_total[c]).abs()).fold(0.0, f64::max);
if scale > 0.0 && imbalance > 1e-6 * scale {
warnings.push(format!("loads and reactions differ by {imbalance:.3e} (relative {:.1e})", imbalance / scale));
}
Ok(StaticResult {
step: step.name.clone(),
nodes: mesh.labels.clone(),
displacement,
reaction,
stress,
von_mises,
elements,
applied_total,
reaction_total,
stats: Stats { dofs: mesh.dofs(), equations: neq, factor_entries: chol.entries(), lanczos_vectors: 0 },
warnings,
})
}
struct ShiftInvert<'a> {
m: &'a Csr,
factor: &'a Factor,
}
impl Operator for ShiftInvert<'_> {
fn n(&self) -> usize {
self.m.n
}
fn mass(&self, x: &[f64], y: &mut [f64]) {
self.m.mul(x, y);
}
fn solve(&self, x: &mut [f64]) -> Result<()> {
self.factor.solve(x)
}
}
/// Block size of the Lanczos iteration: enough for the six rigid-body modes of a free body.
const BLOCK: usize = 6;
/// Relative residual of an accepted Ritz pair.
const TOLERANCE: f64 = 1e-9;
/// Solve a frequency step (the step named `step`, or the model's only frequency step): the
/// lowest natural modes within the step's frequency range.
pub fn solve_frequency(model: &Model, step: Option<&str>, options: &FrequencyOptions, limits: &Limits) -> Result<FrequencyResult> {
let resolved: Resolved = model.resolve()?;
let step = select_step(model, step, |p| matches!(p, Procedure::Frequency { .. }), "frequency")?;
let Procedure::Frequency { modes, min_hz, max_hz } = step.procedure else {
return Err(Error::Internal("frequency step".into()));
};
if let Some(s) = options.shift
&& !s.is_finite()
{
return Err(Error::Invalid(format!("the shift must be a finite number, got {s}")));
}
let mesh = Mesh::new(model, &resolved, limits.max_dofs)?;
let fixed = prescribed(model, &resolved, &mesh, step, false)?;
let graph = NodeGraph::new(mesh.labels.len(), mesh.elements.iter().map(|e| e.nodes.as_slice()));
let Assembled { k, m } = assemble(&mesh, &graph, Some(options.mass))?;
let m = m.ok_or_else(|| Error::Internal("mass matrix".into()))?;
// Every element's mass entries sum to its mass, once per direction.
let total_mass = m.val.iter().sum::<f64>() / 3.0;
let (map, neq) = equations(&nested_dissection(&mesh.xyz, &graph.adjacency), &fixed);
if neq == 0 {
return Err(Error::Invalid("every degree of freedom is held; there is nothing to vibrate".into()));
}
let kff = k.restrict(&map, neq);
let mff = m.restrict(&map, neq);
drop((k, m));
let mut warnings: Vec<String> = resolved.warnings.iter().map(ToString::to_string).collect();
let shifted = |s: f64| -> Result<Factor> { factor_raw(&kff.add_scaled(-s, &mff)?, limits).map_err(|e| factor_error(e, &mesh, &map)) };
let (shift, chol) = match options.shift {
Some(s) => (s, shifted(s)?),
None => match factor_raw(&kff, limits) {
Ok(f) => (0.0, f),
Err(FactorError::NotPositiveDefinite { .. }) => {
// A free (or partly free) body: shift below zero so the rigid-body modes come out.
let (tk, tm): (f64, f64) = (kff.diagonal().iter().sum(), mff.diagonal().iter().sum());
if !(tk > 0.0 && tm > 0.0) {
return Err(Error::Singular("the stiffness or mass has no positive diagonal".into()));
}
let s = -1e-6 * tk / tm;
warnings.push("the structure is not fully supported; rigid-body modes appear at (near) zero frequency".into());
(s, shifted(s)?)
}
Err(e) => return Err(factor_error(e, &mesh, &map)),
},
};
drop(kff);
let two_pi = 2.0 * std::f64::consts::PI;
let wanted = Wanted {
count: usize::try_from(modes).unwrap_or(usize::MAX).min(neq),
min: min_hz.map_or(f64::NEG_INFINITY, |f| (two_pi * f).powi(2)),
max: max_hz.map_or(f64::INFINITY, |f| (two_pi * f).powi(2)),
};
// The basis (vectors and their mass products) costs 2 n × vectors; cap it with the factor's
// entry limit.
let by_memory = limits.max_factor_entries / (2 * neq).max(1);
let max_basis = limits.max_lanczos_vectors.min(by_memory).max(BLOCK.min(neq));
let op = ShiftInvert { m: &mff, factor: &chol };
let pairs = lanczos(&op, shift, wanted, BLOCK, max_basis, TOLERANCE)?;
// Participation: Γ_d = φᵀ M r_d with r_d the unit translation along d on the free dofs.
let mr: Vec<Vec<f64>> = (0..3)
.map(|d| {
let mut r = vec![0.0; neq];
for (dof, mm) in map.iter().enumerate() {
if let Some(x) = mm.filter(|_| dof % 3 == d).and_then(|eq| r.get_mut(eq)) {
*x = 1.0;
}
}
let mut y = vec![0.0; neq];
mff.mul(&r, &mut y);
y
})
.collect();
let mut out = Vec::with_capacity(pairs.values.len());
for (lambda, phi) in pairs.values.iter().zip(&pairs.vectors) {
let participation = [0, 1, 2].map(|d| mr.get(d).map_or(0.0, |y| y.iter().zip(phi).map(|(a, b)| a * b).sum()));
out.push(Mode {
eigenvalue: *lambda,
frequency: lambda.max(0.0).sqrt() / two_pi,
shape: per_node(phi, &map, vec![0.0; mesh.dofs()]),
participation,
effective_mass: participation.map(|g| g * g),
});
}
if out.len() < wanted.count && max_hz.is_none() {
warnings.push(format!("found {} of the {modes} modes asked for", out.len()));
}
Ok(FrequencyResult {
step: step.name.clone(),
nodes: mesh.labels.clone(),
modes: out,
total_mass,
stats: Stats { dofs: mesh.dofs(), equations: neq, factor_entries: chol.entries(), lanczos_vectors: pairs.basis },
warnings,
})
}
/// The result of one step, as a session keeps it.
#[derive(Debug, Clone, PartialEq)]
pub enum StepResult {
Static(StaticResult),
Frequency(FrequencyResult),
}
impl StepResult {
pub fn step(&self) -> &str {
match self {
StepResult::Static(r) => &r.step,
StepResult::Frequency(r) => &r.step,
}
}
pub fn nodes(&self) -> &[u32] {
match self {
StepResult::Static(r) => &r.nodes,
StepResult::Frequency(r) => &r.nodes,
}
}
}
+326
View File
@@ -0,0 +1,326 @@
//! Sparse Cholesky factorization A = L Lᵀ of a symmetric positive definite matrix.
//!
//! The up-looking method of T. A. Davis, *Direct Methods for Sparse Linear Systems*, SIAM 2006,
//! §4.1–4.8: the elimination tree (J. W. H. Liu, *The role of elimination trees in sparse
//! factorization*, SIAM J. Matrix Anal. Appl. 11(1):134–172, 1990) gives the pattern of each row
//! of L as a reach in the tree, the symbolic pass counts every column before any value is
//! computed (so the factor's size is checked against a cap before memory is committed), and each
//! row of L is a sparse triangular solve. Operations run in a fixed order, with no threads and no
//! data-dependent reduction order, so the factor is the same bit for bit on every platform.
//!
//! A pivot at or below `PIVOT_TOLERANCE` times the matrix's own diagonal entry means the matrix
//! is singular to working precision (an unconstrained rigid-body motion, a disconnected part, a
//! zero-stiffness direction); the factorization stops and names the column.
use crate::{Error, Result};
/// Relative pivot size below which the matrix counts as singular.
pub const PIVOT_TOLERANCE: f64 = 1e-10;
/// The upper triangle of a symmetric matrix by columns: column k holds A(i, k) for i ≤ k, rows
/// sorted.
#[derive(Debug, Clone)]
pub struct UpperColumns {
pub n: usize,
pub ptr: Vec<usize>,
pub idx: Vec<usize>,
pub val: Vec<f64>,
}
impl UpperColumns {
/// From a symmetric matrix stored by full rows (row k's entries with column ≤ k are column k
/// of the upper triangle).
pub fn from_symmetric(a: &crate::sparse::Csr) -> UpperColumns {
let mut ptr = Vec::with_capacity(a.n + 1);
ptr.push(0);
let mut idx = Vec::new();
let mut val = Vec::new();
for k in 0..a.n {
let (cols, vals) = a.row(k);
for (c, v) in cols.iter().zip(vals) {
if *c <= k {
idx.push(*c);
val.push(*v);
}
}
ptr.push(idx.len());
}
UpperColumns { n: a.n, ptr, idx, val }
}
fn column(&self, k: usize) -> (&[usize], &[f64]) {
let (a, b) = (self.ptr.get(k).copied().unwrap_or(0), self.ptr.get(k + 1).copied().unwrap_or(0));
(self.idx.get(a..b).unwrap_or_default(), self.val.get(a..b).unwrap_or_default())
}
}
const NONE: usize = usize::MAX;
/// The elimination tree: parent of each column, `NONE` at roots.
fn etree(a: &UpperColumns) -> Vec<usize> {
let mut parent = vec![NONE; a.n];
let mut ancestor = vec![NONE; a.n];
for k in 0..a.n {
let (rows, _) = a.column(k);
for &i0 in rows {
let mut i = i0;
// Walk from i up to the root of its current subtree, compressing the path to k.
while i != NONE && i < k {
let next = ancestor.get(i).copied().unwrap_or(NONE);
if let Some(x) = ancestor.get_mut(i) {
*x = k;
}
if next == NONE
&& let Some(p) = parent.get_mut(i)
{
*p = k;
}
i = next;
}
}
}
parent
}
/// The pattern of row k of L (excluding the diagonal): the reach of column k's entries in the
/// elimination tree. Fills `stack[top..]` in topological order and returns `top`; `mark` holds
/// `k` for visited columns.
fn ereach(a: &UpperColumns, k: usize, parent: &[usize], stack: &mut [usize], mark: &mut [usize], path: &mut Vec<usize>) -> usize {
let n = a.n;
let mut top = n;
if let Some(m) = mark.get_mut(k) {
*m = k;
}
let (rows, _) = a.column(k);
for &i0 in rows {
let mut i = i0;
if i > k {
continue;
}
path.clear();
while i != NONE && mark.get(i).copied() != Some(k) {
path.push(i);
if let Some(m) = mark.get_mut(i) {
*m = k;
}
i = parent.get(i).copied().unwrap_or(NONE);
}
while let Some(v) = path.pop() {
top -= 1;
if let Some(s) = stack.get_mut(top) {
*s = v;
}
}
}
top
}
/// A Cholesky factor, L by columns with the diagonal first in each column.
#[derive(Debug, Clone)]
pub struct Factor {
pub n: usize,
ptr: Vec<usize>,
idx: Vec<usize>,
val: Vec<f64>,
}
/// Why a factorization stopped.
#[derive(Debug, Clone, PartialEq)]
pub enum FactorError {
/// The pivot of this column is not positive (relative to the diagonal).
NotPositiveDefinite { column: usize },
/// The factor would hold more entries than allowed.
TooLarge { entries: usize, limit: usize },
}
impl Factor {
/// The elimination tree and the entry count of each column of L, without computing values.
fn symbolic(a: &UpperColumns) -> (Vec<usize>, Vec<usize>) {
let parent = etree(a);
let mut counts = vec![1usize; a.n];
let mut stack = vec![0; a.n];
let mut mark = vec![NONE; a.n];
let mut path = Vec::new();
for k in 0..a.n {
let top = ereach(a, k, &parent, &mut stack, &mut mark, &mut path);
for &j in stack.get(top..).unwrap_or_default() {
if let Some(c) = counts.get_mut(j) {
*c += 1;
}
}
}
(parent, counts)
}
pub fn new(a: &UpperColumns, max_entries: usize) -> std::result::Result<Factor, FactorError> {
let n = a.n;
let (parent, counts) = Factor::symbolic(a);
let total: usize = counts.iter().sum();
if total > max_entries {
return Err(FactorError::TooLarge { entries: total, limit: max_entries });
}
let mut ptr = Vec::with_capacity(n + 1);
ptr.push(0);
for c in &counts {
ptr.push(ptr.last().copied().unwrap_or(0) + c);
}
let mut idx = vec![0usize; total];
let mut val = vec![0.0f64; total];
// Next free slot in each column.
let mut next: Vec<usize> = ptr.get(..n).unwrap_or_default().to_vec();
let mut x = vec![0.0f64; n];
let mut stack = vec![0usize; n];
let mut mark = vec![NONE; n];
let mut path = Vec::new();
for k in 0..n {
let top = ereach(a, k, &parent, &mut stack, &mut mark, &mut path);
let (rows, vals) = a.column(k);
let mut diag = 0.0;
for (i, v) in rows.iter().zip(vals) {
if *i < k {
if let Some(xi) = x.get_mut(*i) {
*xi = *v;
}
} else if *i == k {
diag = *v;
}
}
let mut d = diag;
for &i in stack.get(top..).unwrap_or_default() {
let start = ptr.get(i).copied().unwrap_or(0);
let lii = val.get(start).copied().unwrap_or(1.0);
let lki = x.get(i).copied().unwrap_or(0.0) / lii;
if let Some(xi) = x.get_mut(i) {
*xi = 0.0;
}
let end = next.get(i).copied().unwrap_or(start);
for p in start + 1..end {
let (r, l) = (idx.get(p).copied().unwrap_or(0), val.get(p).copied().unwrap_or(0.0));
if let Some(xr) = x.get_mut(r) {
*xr -= l * lki;
}
}
d -= lki * lki;
if let Some(slot) = next.get_mut(i) {
if let (Some(ri), Some(vi)) = (idx.get_mut(*slot), val.get_mut(*slot)) {
*ri = k;
*vi = lki;
}
*slot += 1;
}
}
if !(d > PIVOT_TOLERANCE * diag.abs()) || !d.is_finite() {
return Err(FactorError::NotPositiveDefinite { column: k });
}
if let Some(slot) = next.get_mut(k) {
if let (Some(ri), Some(vi)) = (idx.get_mut(*slot), val.get_mut(*slot)) {
*ri = k;
*vi = d.sqrt();
}
*slot += 1;
}
}
Ok(Factor { n, ptr, idx, val })
}
/// Entries in L.
pub fn entries(&self) -> usize {
self.val.len()
}
/// Solve A x = b in place.
pub fn solve(&self, b: &mut [f64]) -> Result<()> {
if b.len() != self.n {
return Err(Error::Internal("right-hand side length".into()));
}
// L y = b, by columns.
for j in 0..self.n {
let (start, end) = (self.ptr.get(j).copied().unwrap_or(0), self.ptr.get(j + 1).copied().unwrap_or(0));
let yj = b.get(j).copied().unwrap_or(0.0) / self.val.get(start).copied().unwrap_or(1.0);
if let Some(x) = b.get_mut(j) {
*x = yj;
}
for p in start + 1..end {
let (r, l) = (self.idx.get(p).copied().unwrap_or(0), self.val.get(p).copied().unwrap_or(0.0));
if let Some(x) = b.get_mut(r) {
*x -= l * yj;
}
}
}
// Lᵀ x = y.
for j in (0..self.n).rev() {
let (start, end) = (self.ptr.get(j).copied().unwrap_or(0), self.ptr.get(j + 1).copied().unwrap_or(0));
let mut s = b.get(j).copied().unwrap_or(0.0);
for p in start + 1..end {
let (r, l) = (self.idx.get(p).copied().unwrap_or(0), self.val.get(p).copied().unwrap_or(0.0));
s -= l * b.get(r).copied().unwrap_or(0.0);
}
if let Some(x) = b.get_mut(j) {
*x = s / self.val.get(start).copied().unwrap_or(1.0);
}
}
Ok(())
}
}
#[cfg(test)]
mod tests {
use super::*;
use crate::sparse::Csr;
fn dense_to_csr(a: &[Vec<f64>]) -> Csr {
let n = a.len();
let mut ptr = vec![0];
let mut idx = Vec::new();
let mut val = Vec::new();
for row in a {
for (j, v) in row.iter().enumerate() {
if *v != 0.0 {
idx.push(j);
val.push(*v);
}
}
ptr.push(idx.len());
}
Csr { n, ptr, idx, val }
}
#[test]
fn factor_and_solve_a_sparse_spd_matrix() {
// A 2D Laplacian-like matrix on a 7 × 5 grid plus a diagonal shift: sparse with fill.
let (w, h) = (7, 5);
let n = w * h;
let mut a = vec![vec![0.0; n]; n];
for i in 0..w {
for j in 0..h {
let k = i * h + j;
a[k][k] = 4.5;
if i + 1 < w {
a[k][k + h] = -1.0;
a[k + h][k] = -1.0;
}
if j + 1 < h {
a[k][k + 1] = -1.0;
a[k + 1][k] = -1.0;
}
}
}
let csr = dense_to_csr(&a);
let f = Factor::new(&UpperColumns::from_symmetric(&csr), usize::MAX).unwrap();
let x: Vec<f64> = (0..n).map(|i| (i as f64 * 0.37).sin()).collect();
let mut b = vec![0.0; n];
csr.mul(&x, &mut b);
f.solve(&mut b).unwrap();
assert!(b.iter().zip(&x).all(|(p, q)| (p - q).abs() < 1e-13), "{b:?}");
// The cap is checked before the numeric factorization.
assert!(matches!(Factor::new(&UpperColumns::from_symmetric(&csr), 10), Err(FactorError::TooLarge { .. })));
// A singular matrix (a pure Laplacian has the constant vector in its null space).
let mut sing = a.clone();
for (k, row) in sing.iter_mut().enumerate() {
let off: f64 = row.iter().enumerate().filter(|(j, _)| *j != k).map(|(_, v)| -v).sum();
row[k] = off;
}
let e = Factor::new(&UpperColumns::from_symmetric(&dense_to_csr(&sing)), usize::MAX).unwrap_err();
assert_eq!(e, FactorError::NotPositiveDefinite { column: n - 1 });
}
}
+521
View File
@@ -0,0 +1,521 @@
//! Eigenvalues: the dense symmetric eigenproblem of the Lanczos projection, and the shifted
//! block Lanczos method for the lowest modes of K φ = λ M φ.
//!
//! **Dense.** Householder reduction to tridiagonal form, then the implicit symmetric QR
//! algorithm with Wilkinson shifts, accumulating the transformations (G. H. Golub, C. F. Van
//! Loan, *Matrix Computations*, 4th ed., Johns Hopkins 2013, §8.3, algorithms 8.3.1 and 8.3.3).
//!
//! **Sparse.** The spectral transformation (T. Ericsson, A. Ruhe, *The spectral transformation
//! Lanczos method for the numerical solution of large sparse generalized symmetric eigenvalue
//! problems*, Math. Comp. 35(152):1251–1268, 1980): with a shift σ below the wanted
//! eigenvalues, the operator (K − σM)⁻¹M is symmetric in the M inner product and has eigenvalues
//! θ = 1/(λ − σ), so the lowest λ become the largest, well separated θ. A block of vectors
//! (R. G. Grimes, J. G. Lewis, H. D. Simon, *A shifted block Lanczos algorithm for solving
//! sparse symmetric generalized eigenproblems*, SIAM J. Matrix Anal. Appl. 15(1):228–272, 1994)
//! finds repeated eigenvalues up to the block size, such as the six rigid-body modes of a free
//! body. Every new block is reorthogonalized against all earlier ones, twice (full
//! reorthogonalization, B. N. Parlett, *The Symmetric Eigenvalue Problem*, SIAM 1998, ch. 13),
//! so no spurious copies appear. A Ritz pair has converged when its residual bound
//! ‖B_{j+1} s‖ is below a relative tolerance. The start block is pseudo-random from a fixed seed,
//! so results are reproducible.
use crate::{Error, Result};
/// Eigenvalues (ascending) and eigenvectors (column k of the row-major `vectors`) of a dense
/// symmetric matrix (row-major, n × n).
pub fn symmetric_eigen(a: &[f64], n: usize) -> Result<(Vec<f64>, Vec<f64>)> {
if a.len() != n * n {
return Err(Error::Internal("dense eigenproblem size".into()));
}
let mut t = a.to_vec();
let mut q = vec![0.0; n * n];
for i in 0..n {
q[i * n + i] = 1.0;
}
// Householder tridiagonalization: for each column k, reflect A[k+1.., k] onto e1.
let mut v = vec![0.0; n];
let mut p = vec![0.0; n];
for k in 0..n.saturating_sub(2) {
let m = k + 1;
let norm: f64 = (m..n).map(|i| t[i * n + k] * t[i * n + k]).sum::<f64>().sqrt();
if norm == 0.0 {
continue;
}
let x0 = t[m * n + k];
let alpha = if x0 >= 0.0 { -norm } else { norm };
for i in m..n {
v[i] = t[i * n + k];
}
v[m] -= alpha;
let vnorm: f64 = (m..n).map(|i| v[i] * v[i]).sum::<f64>().sqrt();
if vnorm == 0.0 {
continue;
}
for i in m..n {
v[i] /= vnorm;
}
// p = A22 v, w = p − (vᵀp) v, A22 −= 2 (v wᵀ + w vᵀ).
for i in m..n {
p[i] = (m..n).map(|j| t[i * n + j] * v[j]).sum();
}
let kk: f64 = (m..n).map(|i| v[i] * p[i]).sum();
for i in m..n {
p[i] -= kk * v[i];
}
for i in m..n {
for j in m..n {
t[i * n + j] -= 2.0 * (v[i] * p[j] + p[i] * v[j]);
}
}
t[m * n + k] = alpha;
t[k * n + m] = alpha;
for i in m + 1..n {
t[i * n + k] = 0.0;
t[k * n + i] = 0.0;
}
// Q = Q (I − 2 v vᵀ).
for r in 0..n {
let s: f64 = (m..n).map(|j| q[r * n + j] * v[j]).sum();
for j in m..n {
q[r * n + j] -= 2.0 * s * v[j];
}
}
}
let mut d: Vec<f64> = (0..n).map(|i| t[i * n + i]).collect();
let mut e: Vec<f64> = (0..n.saturating_sub(1)).map(|i| t[(i + 1) * n + i]).collect();
tridiagonal_qr(&mut d, &mut e, &mut q, n)?;
// Sort ascending, carrying the vectors.
let mut order: Vec<usize> = (0..n).collect();
order.sort_by(|&a, &b| d[a].total_cmp(&d[b]).then(a.cmp(&b)));
let values = order.iter().map(|&i| d[i]).collect();
let mut vectors = vec![0.0; n * n];
for (new, &old) in order.iter().enumerate() {
for r in 0..n {
vectors[r * n + new] = q[r * n + old];
}
}
Ok((values, vectors))
}
/// Diagonalize a symmetric tridiagonal matrix (diagonal d, sub-diagonal e) by implicit QR steps
/// with Wilkinson shifts, applying the rotations to the columns of q.
fn tridiagonal_qr(d: &mut [f64], e: &mut [f64], q: &mut [f64], n: usize) -> Result<()> {
let small = |e: f64, a: f64, b: f64| e.abs() <= f64::EPSILON * (a.abs() + b.abs());
let mut h = n.saturating_sub(1);
let mut iterations = 0usize;
let cap = 30 * n.max(1) + 30;
while h > 0 {
if small(e[h - 1], d[h - 1], d[h]) {
e[h - 1] = 0.0;
h -= 1;
continue;
}
let mut l = h - 1;
while l > 0 && !small(e[l - 1], d[l - 1], d[l]) {
l -= 1;
}
if l > 0 {
e[l - 1] = 0.0;
}
iterations += 1;
if iterations > cap {
return Err(Error::NotConverged("the tridiagonal QR iteration did not converge".into()));
}
// Wilkinson shift from the trailing 2 × 2 block.
let dd = (d[h - 1] - d[h]) / 2.0;
let eh = e[h - 1];
let sign = if dd >= 0.0 { 1.0 } else { -1.0 };
let mu = d[h] - eh * eh / (dd + sign * dd.hypot(eh));
let mut x = d[l] - mu;
let mut z = e[l];
for k in l..h {
let r = x.hypot(z);
let (c, s) = if r == 0.0 { (1.0, 0.0) } else { (x / r, -z / r) };
if k > l {
e[k - 1] = c * e[k - 1] - s * z;
}
let (a, b, dq) = (d[k], e[k], d[k + 1]);
d[k] = c * c * a - 2.0 * c * s * b + s * s * dq;
d[k + 1] = s * s * a + 2.0 * c * s * b + c * c * dq;
e[k] = c * s * (a - dq) + (c * c - s * s) * b;
if k + 1 < h {
z = -s * e[k + 1];
e[k + 1] *= c;
x = e[k];
}
for row in 0..n {
let (qp, qq) = (q[row * n + k], q[row * n + k + 1]);
q[row * n + k] = c * qp - s * qq;
q[row * n + k + 1] = s * qp + c * qq;
}
}
}
Ok(())
}
/// A small deterministic pseudo-random generator (xorshift64*, S. Vigna, *An experimental
/// exploration of Marsaglia's xorshift generators, scrambled*, ACM TOMS 42(4), 2016) for
/// Lanczos start vectors.
pub struct Random(u64);
impl Random {
pub fn new(seed: u64) -> Random {
Random(seed.max(1))
}
/// Uniform in [−1, 1).
pub fn uniform(&mut self) -> f64 {
self.0 ^= self.0 >> 12;
self.0 ^= self.0 << 25;
self.0 ^= self.0 >> 27;
let v = self.0.wrapping_mul(0x2545_f491_4f6c_dd1d);
(v >> 11) as f64 / (1u64 << 52) as f64 - 1.0
}
}
/// What the Lanczos iteration looks for, in terms of λ = σ + 1/θ.
#[derive(Debug, Clone, Copy)]
pub struct Wanted {
/// Modes to return within the range.
pub count: usize,
/// Lower and upper bounds on λ (eigenvalues outside are skipped).
pub min: f64,
pub max: f64,
}
/// The operators the Lanczos iteration needs.
pub trait Operator {
fn n(&self) -> usize;
/// y = M x.
fn mass(&self, x: &[f64], y: &mut [f64]);
/// x ← (K − σM)⁻¹ x.
fn solve(&self, x: &mut [f64]) -> Result<()>;
}
/// Converged eigenpairs: λ ascending, vectors M-orthonormal.
#[derive(Debug, Clone)]
pub struct Eigenpairs {
pub values: Vec<f64>,
pub vectors: Vec<Vec<f64>>,
/// Lanczos vectors used.
pub basis: usize,
}
fn dot(a: &[f64], b: &[f64]) -> f64 {
a.iter().zip(b).map(|(x, y)| x * y).sum()
}
/// Orthonormalize a block against the basis and itself in the M inner product (classical
/// Gram–Schmidt, twice). A column that vanishes is replaced by a fresh random direction and its
/// diagonal coefficient stays zero. Returns the new vectors, their M products and the
/// upper-triangular coefficients `r[j][i]` of column i on new vector j.
fn orthonormalize(
op: &impl Operator,
w: Vec<Vec<f64>>,
q: &[Vec<f64>],
mq: &[Vec<f64>],
rng: &mut Random,
scratch: &mut [f64],
) -> (Vec<Vec<f64>>, Vec<Vec<f64>>, Vec<Vec<f64>>) {
let n = op.n();
let k = w.len();
let mut r = vec![vec![0.0; k]; k];
let mut out: Vec<Vec<f64>> = Vec::with_capacity(k);
let mut mout: Vec<Vec<f64>> = Vec::with_capacity(k);
for (i, mut v) in w.into_iter().enumerate() {
let mut fresh = false;
for _attempt in 0..4 {
op.mass(&v, scratch);
let before = dot(&v, scratch).max(0.0).sqrt();
for _ in 0..2 {
for (qj, mqj) in q.iter().zip(mq) {
let c = dot(mqj, &v);
v.iter_mut().zip(qj).for_each(|(x, y)| *x -= c * y);
}
for (j, (qj, mqj)) in out.iter().zip(&mout).enumerate() {
let c = dot(mqj, &v);
v.iter_mut().zip(qj).for_each(|(x, y)| *x -= c * y);
if !fresh && let Some(x) = r.get_mut(j).and_then(|row| row.get_mut(i)) {
*x += c;
}
}
}
op.mass(&v, scratch);
let norm = dot(&v, scratch).max(0.0).sqrt();
if norm > 1e-8 * before && norm > 0.0 {
if !fresh && let Some(x) = r.get_mut(i).and_then(|row| row.get_mut(i)) {
*x = norm;
}
v.iter_mut().for_each(|x| *x /= norm);
mout.push(scratch.iter().map(|x| x / norm).collect());
out.push(v);
break;
}
fresh = true;
v = (0..n).map(|_| rng.uniform()).collect();
}
}
(out, mout, r)
}
/// Shift-invert block Lanczos with full reorthogonalization.
pub fn lanczos(op: &impl Operator, shift: f64, wanted: Wanted, block: usize, max_basis: usize, tolerance: f64) -> Result<Eigenpairs> {
let n = op.n();
if n == 0 {
return Err(Error::Invalid("there are no free degrees of freedom".into()));
}
let b = block.clamp(1, n);
let max_basis = max_basis.min(n).max(b);
let mut rng = Random::new(0x9e37_79b9_7f4a_7c15);
let mut q: Vec<Vec<f64>> = Vec::new();
let mut mq: Vec<Vec<f64>> = Vec::new();
// The projected matrix T, grown block by block (row-major in a growing square).
let mut t: Vec<Vec<f64>> = Vec::new();
let mut scratch = vec![0.0; n];
// Start block.
let start: Vec<Vec<f64>> = (0..b).map(|_| (0..n).map(|_| rng.uniform()).collect()).collect();
let (mut cur, mut mcur, _) = orthonormalize(op, start, &q, &mq, &mut rng, &mut scratch);
if cur.len() < b {
return Err(Error::NotConverged("could not build a Lanczos start block".into()));
}
let mut prev_b: Option<Vec<Vec<f64>>> = None;
let mut next_check = (wanted.count + b).max(2 * b);
loop {
let j0 = q.len();
// W = Op Q_j.
let mut w: Vec<Vec<f64>> = Vec::with_capacity(b);
for mx in &mcur {
let mut y = mx.clone();
op.solve(&mut y)?;
w.push(y);
}
// A_j = Q_jᵀ M W (symmetrized), W −= Q_j A_j (the earlier blocks go in the full
// reorthogonalization below).
let mut a = vec![vec![0.0; b]; b];
for (i, mqi) in mcur.iter().enumerate() {
for (j, wj) in w.iter().enumerate() {
a[i][j] = dot(mqi, wj);
}
}
for i in 0..b {
for j in i + 1..b {
let s = 0.5 * (a[i][j] + a[j][i]);
a[i][j] = s;
a[j][i] = s;
}
}
q.append(&mut cur);
mq.append(&mut mcur);
let m = q.len();
for row in &mut t {
row.resize(m, 0.0);
}
t.resize(m, vec![0.0; m]);
for i in 0..b {
for j in 0..b {
t[j0 + i][j0 + j] = a[i][j];
}
}
if let Some(bp) = &prev_b {
// T[block j][block j−1] = B_j, T[block j−1][block j] = B_jᵀ.
for i in 0..b {
for j in 0..b {
t[j0 + i][j0 - b + j] = bp[i][j];
t[j0 - b + j][j0 + i] = bp[i][j];
}
}
}
// Full reorthogonalization happens inside the QR against the whole basis.
let full = m >= max_basis || m + b > n;
let (next, mnext, bnext) =
if full { (Vec::new(), Vec::new(), vec![vec![0.0; b]; b]) } else { orthonormalize(op, w, &q, &mq, &mut rng, &mut scratch) };
// Convergence check on a schedule (the dense eigenproblem costs m³).
if m >= next_check || full || next.len() < b {
next_check = m + (m / 4).max(b);
let dense: Vec<f64> = t.iter().flatten().copied().collect();
let (theta, s) = symmetric_eigen(&dense, m)?;
// Order by λ ascending = θ descending (θ > 0 below the spectrum).
let mut idx: Vec<usize> = (0..m).collect();
idx.sort_by(|&x, &y| theta[y].total_cmp(&theta[x]).then(x.cmp(&y)));
let mut done = false;
let mut accepted = Vec::new();
let mut found = 0;
for &i in &idx {
let th = theta[i];
if !(th > 0.0) {
break;
}
// Residual bound ‖B_{j+1} s_last‖ with s_last the last block of the Ritz vector.
let mut res2 = 0.0;
if !full {
for r in 0..b {
let v: f64 = (0..b).map(|c| bnext[r][c] * s[(m - b + c) * m + i]).sum();
res2 += v * v;
}
}
if res2.sqrt() > tolerance * th {
break;
}
let lambda = shift + 1.0 / th;
if lambda > wanted.max {
done = true;
break;
}
if lambda >= wanted.min {
accepted.push(i);
found += 1;
if found == wanted.count {
done = true;
break;
}
}
}
if full && !done {
if m >= n {
done = true;
} else {
return Err(Error::NotConverged(format!(
"found {found} of {} modes after {m} Lanczos vectors (the cap); raise the iteration limit or ask for fewer modes",
wanted.count
)));
}
}
if done {
let mut values = Vec::new();
let mut vectors = Vec::new();
for &i in &accepted {
values.push(shift + 1.0 / theta[i]);
let mut x = vec![0.0; n];
for (k, qk) in q.iter().enumerate() {
let c = s[k * m + i];
x.iter_mut().zip(qk).for_each(|(a, b)| *a += c * b);
}
op.mass(&x, &mut scratch);
let norm = dot(&x, &scratch).max(0.0).sqrt();
if norm > 0.0 {
x.iter_mut().for_each(|a| *a /= norm);
}
// Deterministic sign: the largest component positive.
let big = x.iter().copied().fold(0.0f64, |m, v| if v.abs() > m.abs() { v } else { m });
if big < 0.0 {
x.iter_mut().for_each(|a| *a = -*a);
}
vectors.push(x);
}
return Ok(Eigenpairs { values, vectors, basis: m });
}
}
if full {
return Err(Error::NotConverged("the Lanczos basis is exhausted".into()));
}
cur = next;
mcur = mnext;
if cur.len() < b {
return Err(Error::NotConverged("the Lanczos block lost rank".into()));
}
prev_b = Some(bnext);
}
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn dense_symmetric_eigen() {
let n = 9;
let mut rng = Random::new(7);
let mut a = vec![0.0; n * n];
for i in 0..n {
for j in 0..=i {
let v = rng.uniform();
a[i * n + j] = v;
a[j * n + i] = v;
}
}
let (values, vectors) = symmetric_eigen(&a, n).unwrap();
assert!(values.windows(2).all(|w| w[0] <= w[1]));
for k in 0..n {
for i in 0..n {
let av: f64 = (0..n).map(|j| a[i * n + j] * vectors[j * n + k]).sum();
assert!((av - values[k] * vectors[i * n + k]).abs() < 1e-12, "pair {k}");
}
let norm: f64 = (0..n).map(|i| vectors[i * n + k].powi(2)).sum();
assert!((norm - 1.0).abs() < 1e-12);
}
assert_eq!(symmetric_eigen(&[3.0], 1).unwrap().0, vec![3.0]);
}
/// K and M diagonal.
struct Diagonal {
k: Vec<f64>,
m: Vec<f64>,
shift: f64,
}
impl Operator for Diagonal {
fn n(&self) -> usize {
self.k.len()
}
fn mass(&self, x: &[f64], y: &mut [f64]) {
for i in 0..x.len() {
y[i] = self.m[i] * x[i];
}
}
fn solve(&self, x: &mut [f64]) -> Result<()> {
for i in 0..x.len() {
x[i] /= self.k[i] - self.shift * self.m[i];
}
Ok(())
}
}
#[test]
fn lanczos_finds_repeated_and_zero_eigenvalues() {
// Six zero eigenvalues, then 1 twice, then distinct values; M not the identity.
let n = 200;
let lambdas: Vec<f64> = (0..n)
.map(|i| {
if i < 6 {
0.0
} else if i < 8 {
1.0
} else {
1.0 + (i - 7) as f64 * 0.5
}
})
.collect();
let m: Vec<f64> = (0..n).map(|i| 1.0 + (i % 7) as f64 * 0.1).collect();
let k: Vec<f64> = lambdas.iter().zip(&m).map(|(l, m)| l * m).collect();
let shift = -1e-3;
let op = Diagonal { k, m, shift };
let wanted = Wanted { count: 10, min: f64::NEG_INFINITY, max: f64::INFINITY };
let pairs = lanczos(&op, shift, wanted, 6, n, 1e-9).unwrap();
assert_eq!(pairs.values.len(), 10);
let want = [0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 1.0, 1.0, 1.5, 2.0];
for (got, w) in pairs.values.iter().zip(want) {
assert!((got - w).abs() < 1e-8, "{:?}", pairs.values);
}
// M-orthonormal vectors.
let mut y = vec![0.0; n];
for a in &pairs.vectors {
for b in &pairs.vectors {
op.mass(b, &mut y);
let d = dot(a, &y);
assert!((d - if std::ptr::eq(a, b) { 1.0 } else { 0.0 }).abs() < 1e-8);
}
}
// A range: values in [1.2, 3.2] (λ), at most 100.
let ranged = lanczos(&op, shift, Wanted { count: 100, min: 1.2, max: 3.2 }, 6, n, 1e-9).unwrap();
assert_eq!(ranged.values.len(), 4, "{:?}", ranged.values);
assert!(ranged.values.iter().zip([1.5, 2.0, 2.5, 3.0]).all(|(g, w)| (g - w).abs() < 1e-8), "{:?}", ranged.values);
// Caps: a basis too small to converge is an error, not a hang.
assert!(lanczos(&op, shift, Wanted { count: 50, min: f64::NEG_INFINITY, max: f64::INFINITY }, 6, 24, 1e-9).is_err());
// Tiny problems: the whole space.
let small = Diagonal { k: vec![2.0, 1.0, 3.0], m: vec![1.0; 3], shift: 0.0 };
let all = lanczos(&small, 0.0, Wanted { count: 5, min: f64::NEG_INFINITY, max: f64::INFINITY }, 6, 100, 1e-9).unwrap();
assert_eq!(all.values.len(), 3);
assert!((all.values[0] - 1.0).abs() < 1e-12 && (all.values[2] - 3.0).abs() < 1e-12, "{:?}", all.values);
}
}
+89
View File
@@ -0,0 +1,89 @@
//! ModelCraft's implicit solver: linear static and frequency analysis of a model's steps.
//!
//! The pipeline, for one step of a [`modelcraft_model::Model`]:
//! 1. **System** ([`system`]): the model is resolved; every section's elements become solid
//! elements with their material's elasticity and the section's formulation
//! ([`modelcraft_fem`] kernels); the step's boundary conditions give the prescribed degrees of
//! freedom, its loads the load vector (forces and tractions as the model distributes them,
//! consistent pressure loads, gravity and body forces).
//! 2. **Assembly** ([`sparse`]) on the node graph, elements in label order.
//! 3. **Ordering** ([`ordering`]): nested dissection of the nodes; the free degrees of freedom
//! are numbered in that order and the prescribed ones eliminated (u_p moved to the right-hand
//! side), with no penalty numbers.
//! 4. **Solution** ([`cholesky`]): sparse Cholesky; reactions K u − f at the prescribed degrees
//! of freedom; stresses at the integration points, extrapolated and averaged at the nodes, and
//! von Mises. Frequency analysis ([`eigen`]) runs shift-invert block Lanczos on the same
//! kind of factorization.
//!
//! Everything is sequential and in a fixed order, so the same model gives the same numbers bit
//! for bit; sizes and iterations are capped by [`Limits`].
#![deny(clippy::unwrap_used, clippy::expect_used, clippy::panic, clippy::unimplemented, clippy::todo, clippy::unreachable)]
#![forbid(unsafe_code)]
// Matrix kernels read as the textbook formulas with index loops.
#![allow(clippy::needless_range_loop)]
pub mod analysis;
pub mod cholesky;
pub mod eigen;
pub mod ordering;
pub mod sparse;
pub mod system;
pub use analysis::{
ElementStress, FrequencyOptions, FrequencyResult, MassKind, Mode, StaticResult, Stats, StepResult, solve_frequency, solve_static,
};
#[derive(Debug, Clone, PartialEq, thiserror::Error)]
pub enum Error {
#[error(transparent)]
Model(#[from] modelcraft_model::Error),
#[error("invalid input: {0}")]
Invalid(String),
#[error("not supported yet: {0}")]
NotSupported(String),
/// An element kernel failed (inverted geometry, a formulation it lacks, …).
#[error("element {label}: {source}")]
Element { label: u32, source: modelcraft_fem::Error },
/// The stiffness (or shifted matrix) is singular.
#[error("{0}")]
Singular(String),
#[error("limit reached: {0}")]
Limit(String),
#[error("did not converge: {0}")]
NotConverged(String),
/// A broken internal invariant (a bug), reported instead of a panic.
#[error("internal error: {0}")]
Internal(String),
}
pub type Result<T> = std::result::Result<T, Error>;
impl Error {
/// A kernel error, naming the element.
pub fn element(label: u32, source: modelcraft_fem::Error) -> Error {
Error::Element { label, source }
}
}
/// Caps on the size of a solution.
#[derive(Debug, Clone, Copy, PartialEq, Eq)]
pub struct Limits {
/// Degrees of freedom of the mesh.
pub max_dofs: usize,
/// Entries of the Cholesky factor (8 bytes each); also bounds the Lanczos basis memory.
pub max_factor_entries: usize,
/// Lanczos vectors (iterations × block size).
pub max_lanczos_vectors: usize,
}
impl Limits {
pub const MAX_DOFS: usize = 6_000_000;
pub const MAX_FACTOR_ENTRIES: usize = 400_000_000;
pub const MAX_LANCZOS_VECTORS: usize = 3_000;
}
impl Default for Limits {
fn default() -> Limits {
Limits { max_dofs: Limits::MAX_DOFS, max_factor_entries: Limits::MAX_FACTOR_ENTRIES, max_lanczos_vectors: Limits::MAX_LANCZOS_VECTORS }
}
}
+119
View File
@@ -0,0 +1,119 @@
//! Fill-reducing ordering: nested dissection by coordinate bisection.
//!
//! Nested dissection (A. George, *Nested dissection of a regular finite element mesh*, SIAM J.
//! Numer. Anal. 10(2):345–363, 1973) orders a separator after the two parts it splits, so the
//! Cholesky factor of a 3D mesh with n nodes fills O(n^{4/3}) instead of the O(n^{5/3}) of a band
//! or envelope ordering. The separator here is geometric: the nodes are split at the median of
//! the longest axis of their bounding box, and the nodes of the smaller side that touch the other
//! side form the separator (the coordinate nested dissection of H. D. Simon, *Partitioning of
//! unstructured problems for parallel processing*, Computing Systems in Engineering 2:135–148,
//! 1991, with vertex separators). Ties are broken by node index, so the ordering is
//! deterministic.
/// Parts this small are ordered as they come.
const LEAF: usize = 16;
/// A permutation of the nodes: `order[k]` is the node eliminated k-th.
pub fn nested_dissection(xyz: &[[f64; 3]], adjacency: &[Vec<usize>]) -> Vec<usize> {
let n = xyz.len();
let mut order = Vec::with_capacity(n);
// 0 = not in the current part, 1 = left, 2 = right.
let mut side = vec![0u8; n];
// An explicit stack instead of recursion: (part, separator to emit after it).
enum Task {
Split(Vec<usize>),
Emit(Vec<usize>),
}
let mut stack = vec![Task::Split((0..n).collect())];
while let Some(task) = stack.pop() {
let mut part = match task {
Task::Emit(sep) => {
order.extend(sep);
continue;
}
Task::Split(p) => p,
};
if part.len() <= LEAF {
order.extend(part);
continue;
}
let mut lo = [f64::INFINITY; 3];
let mut hi = [f64::NEG_INFINITY; 3];
for &v in &part {
let p = xyz.get(v).copied().unwrap_or_default();
for k in 0..3 {
lo[k] = lo[k].min(p[k]);
hi[k] = hi[k].max(p[k]);
}
}
let axis = (0..3).fold(0, |best, k| if hi[k] - lo[k] > hi[best] - lo[best] { k } else { best });
let key = |v: usize| xyz.get(v).map_or(0.0, |p| p[axis]);
part.sort_by(|&a, &b| key(a).total_cmp(&key(b)).then(a.cmp(&b)));
let half = part.len() / 2;
for (i, &v) in part.iter().enumerate() {
if let Some(s) = side.get_mut(v) {
*s = if i < half { 1 } else { 2 };
}
}
let touches = |v: usize, other: u8| adjacency.get(v).is_some_and(|row| row.iter().any(|w| side.get(*w) == Some(&other)));
let (left, right) = part.split_at(half);
let left_boundary: Vec<usize> = left.iter().copied().filter(|&v| touches(v, 2)).collect();
let right_boundary: Vec<usize> = right.iter().copied().filter(|&v| touches(v, 1)).collect();
let separator = if left_boundary.len() <= right_boundary.len() { left_boundary } else { right_boundary };
for &v in &part {
if let Some(s) = side.get_mut(v) {
*s = 0;
}
}
// Mark the separator so the parts leave it out.
for &v in &separator {
if let Some(s) = side.get_mut(v) {
*s = 3;
}
}
let a: Vec<usize> = left.iter().copied().filter(|v| side.get(*v) != Some(&3)).collect();
let b: Vec<usize> = right.iter().copied().filter(|v| side.get(*v) != Some(&3)).collect();
for &v in &separator {
if let Some(s) = side.get_mut(v) {
*s = 0;
}
}
// Order: a, then b, then the separator (the stack runs in reverse).
stack.push(Task::Emit(separator));
stack.push(Task::Split(b));
stack.push(Task::Split(a));
}
order
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn a_permutation_with_separators_last() {
// A 12 × 12 grid graph.
let m = 12;
let id = |i: usize, j: usize| i * m + j;
let xyz: Vec<[f64; 3]> = (0..m * m).map(|v| [(v / m) as f64, (v % m) as f64, 0.0]).collect();
let mut adj = vec![Vec::new(); m * m];
for i in 0..m {
for j in 0..m {
for (di, dj) in [(0i64, 1i64), (1, 0), (0, -1), (-1, 0), (0, 0)] {
let (a, b) = (i as i64 + di, j as i64 + dj);
if (0..m as i64).contains(&a) && (0..m as i64).contains(&b) {
adj[id(i, j)].push(id(a as usize, b as usize));
}
}
}
}
let order = nested_dissection(&xyz, &adj);
let mut sorted = order.clone();
sorted.sort_unstable();
assert_eq!(sorted, (0..m * m).collect::<Vec<_>>());
// The top separator (last 12 entries) is one grid line.
let last: Vec<usize> = order[m * m - m..].to_vec();
assert!(last.iter().all(|v| v / m == last[0] / m) || last.iter().all(|v| v % m == last[0] % m), "{last:?}");
assert_eq!(order, nested_dissection(&xyz, &adj), "deterministic");
}
}
+233
View File
@@ -0,0 +1,233 @@
//! Sparse symmetric matrices in compressed rows, both triangles stored.
//!
//! Assembly works on the node graph: a node's row holds every node it shares an element with,
//! and each node pair is a dense 3 × 3 block, so the pattern is built once from the element
//! connectivity and the stiffness and mass share it. Sums run in a fixed order (elements by
//! label, then the element's own node order), so assembled values are the same bit for bit on
//! every run and platform.
use crate::{Error, Result};
/// A square sparse matrix in compressed rows with sorted column indices.
#[derive(Debug, Clone, PartialEq)]
pub struct Csr {
pub n: usize,
pub ptr: Vec<usize>,
pub idx: Vec<usize>,
pub val: Vec<f64>,
}
impl Csr {
/// The row's column indices and values.
pub fn row(&self, r: usize) -> (&[usize], &[f64]) {
let (a, b) = (self.ptr.get(r).copied().unwrap_or(0), self.ptr.get(r + 1).copied().unwrap_or(0));
(self.idx.get(a..b).unwrap_or_default(), self.val.get(a..b).unwrap_or_default())
}
/// y = A x.
pub fn mul(&self, x: &[f64], y: &mut [f64]) {
for (r, yr) in y.iter_mut().enumerate().take(self.n) {
let (cols, vals) = self.row(r);
*yr = cols.iter().zip(vals).map(|(c, v)| v * x.get(*c).copied().unwrap_or(0.0)).sum();
}
}
pub fn diagonal(&self) -> Vec<f64> {
(0..self.n)
.map(|r| {
let (cols, vals) = self.row(r);
cols.binary_search(&r).ok().and_then(|i| vals.get(i)).copied().unwrap_or(0.0)
})
.collect()
}
/// The matrix on a subset of rows and columns, renumbered: `map[i]` is the new index of old
/// index i, or `None` to drop it. The new rows keep sorted columns.
pub fn restrict(&self, map: &[Option<usize>], n: usize) -> Csr {
let mut rows: Vec<Vec<(usize, f64)>> = vec![Vec::new(); n];
for (r, m) in map.iter().enumerate() {
let Some(nr) = *m else { continue };
let (cols, vals) = self.row(r);
let Some(out) = rows.get_mut(nr) else { continue };
for (c, v) in cols.iter().zip(vals) {
if let Some(Some(nc)) = map.get(*c) {
out.push((*nc, *v));
}
}
out.sort_by_key(|e| e.0);
}
let mut ptr = Vec::with_capacity(n + 1);
ptr.push(0);
let mut idx = Vec::new();
let mut val = Vec::new();
for row in rows {
for (c, v) in row {
idx.push(c);
val.push(v);
}
ptr.push(idx.len());
}
Csr { n, ptr, idx, val }
}
/// `self + a·other` on the same pattern.
pub fn add_scaled(&self, a: f64, other: &Csr) -> Result<Csr> {
if self.ptr != other.ptr || self.idx != other.idx {
return Err(Error::Internal("matrices with different patterns".into()));
}
let val = self.val.iter().zip(&other.val).map(|(x, y)| x + a * y).collect();
Ok(Csr { n: self.n, ptr: self.ptr.clone(), idx: self.idx.clone(), val })
}
}
/// The node-block pattern of a mesh: for each node, the sorted nodes it shares an element with
/// (itself included).
#[derive(Debug, Clone)]
pub struct NodeGraph {
pub adjacency: Vec<Vec<usize>>,
}
impl NodeGraph {
pub fn new(nodes: usize, elements: impl Iterator<Item = impl AsRef<[usize]>>) -> NodeGraph {
let mut adjacency: Vec<Vec<usize>> = vec![Vec::new(); nodes];
for e in elements {
let e = e.as_ref();
for &a in e {
if let Some(row) = adjacency.get_mut(a) {
row.extend_from_slice(e);
}
}
}
for row in &mut adjacency {
row.sort_unstable();
row.dedup();
}
NodeGraph { adjacency }
}
/// Nonzeros of the dof-level matrix (3 × 3 per node pair).
pub fn entries(&self) -> usize {
self.adjacency.iter().map(|r| 9 * r.len()).sum()
}
/// A zero matrix over every degree of freedom (3 per node) on this pattern.
pub fn zero_matrix(&self) -> Csr {
let n = 3 * self.adjacency.len();
let mut ptr = Vec::with_capacity(n + 1);
ptr.push(0);
let mut idx = Vec::with_capacity(self.entries());
for row in &self.adjacency {
for _ in 0..3 {
for &b in row {
idx.extend([3 * b, 3 * b + 1, 3 * b + 2]);
}
ptr.push(idx.len());
}
}
let val = vec![0.0; idx.len()];
Csr { n, ptr, idx, val }
}
}
/// Where node b's 3 × 3 block starts in each of node a's three rows (the rows of a node share
/// one pattern, built by [`NodeGraph::zero_matrix`]): one search per node pair.
fn block_offsets(k: &Csr, a: usize, b: usize) -> Result<[usize; 3]> {
let (start, end) = (k.ptr.get(3 * a).copied().unwrap_or(0), k.ptr.get(3 * a + 1).copied().unwrap_or(0));
let cols = k.idx.get(start..end).ok_or_else(|| Error::Internal("pattern".into()))?;
let at = cols.binary_search(&(3 * b)).map_err(|_| Error::Internal("entry outside the pattern".into()))?;
Ok([0, 1, 2].map(|r| k.ptr.get(3 * a + r).copied().unwrap_or(0) + at))
}
/// Add an element matrix (3n × 3n, row-major, degrees of freedom node by node) into a matrix
/// built by [`NodeGraph::zero_matrix`]; `nodes` are the element's global node indices.
pub fn add_block(k: &mut Csr, nodes: &[usize], data: &[f64]) -> Result<()> {
let width = 3 * nodes.len();
if data.len() != width * width {
return Err(Error::Internal("element matrix size".into()));
}
for (i, &a) in nodes.iter().enumerate() {
for (j, &b) in nodes.iter().enumerate() {
let rows = block_offsets(k, a, b)?;
for (r, start) in rows.iter().enumerate() {
for c in 0..3 {
if let (Some(x), Some(v)) = (k.val.get_mut(start + c), data.get((3 * i + r) * width + 3 * j + c)) {
*x += v;
}
}
}
}
}
Ok(())
}
/// Add an n × n element matrix to each displacement component's block (consistent mass).
pub fn add_scalar(k: &mut Csr, nodes: &[usize], data: &[f64]) -> Result<()> {
let n = nodes.len();
if data.len() != n * n {
return Err(Error::Internal("element matrix size".into()));
}
for (i, &a) in nodes.iter().enumerate() {
for (j, &b) in nodes.iter().enumerate() {
let rows = block_offsets(k, a, b)?;
let v = data.get(i * n + j).copied().unwrap_or(0.0);
for (c, start) in rows.iter().enumerate() {
if let Some(x) = k.val.get_mut(start + c) {
*x += v;
}
}
}
}
Ok(())
}
/// Add a per-node diagonal to each displacement component (lumped mass).
pub fn add_diagonal(k: &mut Csr, nodes: &[usize], diagonal: &[f64]) -> Result<()> {
for (&a, v) in nodes.iter().zip(diagonal) {
let rows = block_offsets(k, a, a)?;
for (c, start) in rows.iter().enumerate() {
if let Some(x) = k.val.get_mut(start + c) {
*x += v;
}
}
}
Ok(())
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn assemble_restrict_multiply() {
// Two "elements" sharing node 1.
let g = NodeGraph::new(3, [vec![0usize, 1], vec![1, 2]].into_iter());
assert_eq!(g.adjacency, vec![vec![0, 1], vec![0, 1, 2], vec![1, 2]]);
let mut k = g.zero_matrix();
let mut e = vec![0.0; 36];
for i in 0..6 {
e[i * 6 + i] = 2.0;
e[i * 6 + (i + 3) % 6] = -1.0;
}
add_block(&mut k, &[0, 1], &e).unwrap();
add_block(&mut k, &[1, 2], &e).unwrap();
assert_eq!(k.diagonal(), vec![2.0, 2.0, 2.0, 4.0, 4.0, 4.0, 2.0, 2.0, 2.0]);
let x = vec![1.0; 9];
let mut y = vec![0.0; 9];
k.mul(&x, &mut y);
assert_eq!(y, vec![1.0; 3].into_iter().chain([2.0; 3]).chain([1.0; 3]).collect::<Vec<_>>());
// Keep the x components only, in reverse order.
let map: Vec<Option<usize>> = (0..9).map(|i| (i % 3 == 0).then_some(2 - i / 3)).collect();
let r = k.restrict(&map, 3);
assert_eq!(r.diagonal(), vec![2.0, 4.0, 2.0]);
assert_eq!(r.row(1).0, &[0, 1, 2]);
assert!(add_block(&mut k, &[0, 2], &e).is_err(), "nodes 0 and 2 share no element");
// Scalar (per component) and diagonal additions land on each component.
let mut m = g.zero_matrix();
add_scalar(&mut m, &[0, 1], &[2.0, 1.0, 1.0, 2.0]).unwrap();
add_diagonal(&mut m, &[2], &[5.0]).unwrap();
assert_eq!(m.diagonal(), vec![2.0, 2.0, 2.0, 2.0, 2.0, 2.0, 5.0, 5.0, 5.0]);
assert_eq!(m.row(0).1, &[2.0, 0.0, 0.0, 1.0, 0.0, 0.0]);
let s = k.add_scaled(-1.0, &k).unwrap();
assert!(s.val.iter().all(|v| *v == 0.0));
}
}
+218
View File
@@ -0,0 +1,218 @@
//! From the resolved model to the discrete system: the solid elements with their materials and
//! formulations, the degrees of freedom, prescribed values and the load vector of a step.
use modelcraft_fem::element::{Formulation, Solid};
use modelcraft_fem::{Elasticity, elasticity, face};
use modelcraft_model::{ElementKind, Load, Model, Resolved, SectionKind, Step, Target};
use crate::{Error, Result};
/// A solid element ready for the kernels.
#[derive(Debug, Clone)]
pub struct Elem {
pub label: u32,
pub kind: ElementKind,
/// Indices into [`Mesh::labels`].
pub nodes: Vec<usize>,
pub xyz: Vec<[f64; 3]>,
pub formulation: Formulation,
pub d: Elasticity,
pub density: Option<f64>,
}
impl Elem {
pub fn solid(&self) -> Result<Solid<'_>> {
Solid::new(self.kind, &self.xyz, self.formulation).map_err(|e| Error::element(self.label, e))
}
}
/// The analysed mesh: the nodes that carry degrees of freedom (those of the solid elements),
/// sorted by label, and the elements sorted by label.
#[derive(Debug, Clone)]
pub struct Mesh {
pub labels: Vec<u32>,
pub xyz: Vec<[f64; 3]>,
pub elements: Vec<Elem>,
}
impl Mesh {
pub fn node(&self, label: u32) -> Option<usize> {
self.labels.binary_search(&label).ok()
}
pub fn element(&self, label: u32) -> Option<&Elem> {
self.elements.binary_search_by_key(&label, |e| e.label).ok().and_then(|i| self.elements.get(i))
}
pub fn dofs(&self) -> usize {
3 * self.labels.len()
}
/// Build it from the model and its resolved view, refusing what the solver cannot represent.
pub fn new(model: &Model, resolved: &Resolved, max_dofs: usize) -> Result<Mesh> {
if let Some(name) = model.couplings().keys().next() {
return Err(Error::NotSupported(format!(
"couplings (coupling `{name}`); the solver handles solid elements without reference points so far"
)));
}
let mut elements = Vec::new();
for (name, section) in model.sections() {
if !matches!(section.kind, SectionKind::Solid {}) {
return Err(Error::NotSupported(format!(
"{} sections (section `{name}`); the solver has solid elements so far",
section.kind.name()
)));
}
let material = model
.material(&section.material)
.ok_or_else(|| Error::Invalid(format!("section `{name}`: material `{}` is missing", section.material)))?;
let elastic =
material.elastic.as_ref().ok_or_else(|| Error::Invalid(format!("material `{}` has no elastic constants", section.material)))?;
let d = elasticity(elastic).map_err(|e| Error::Invalid(format!("material `{}`: {e}", section.material)))?;
let set = resolved.sets.get(&section.set).ok_or_else(|| Error::Invalid(format!("set `{}` is not resolved", section.set)))?;
for &label in &set.elements {
let el = model.element(label).ok_or_else(|| Error::Invalid(format!("element {label} is missing")))?;
let formulation = Formulation::from_section(el.kind, &section.formulation).map_err(|e| Error::element(label, e))?;
elements.push((label, el.kind, el.nodes.clone(), formulation, d, material.density));
}
}
elements.sort_by_key(|e| e.0);
let mut labels: Vec<u32> = elements.iter().flat_map(|e| e.2.iter().copied()).collect();
labels.sort_unstable();
labels.dedup();
if 3 * labels.len() > max_dofs {
return Err(Error::Limit(format!("the model has {} degrees of freedom; the limit is {max_dofs}", 3 * labels.len())));
}
let xyz: Vec<[f64; 3]> = labels
.iter()
.map(|l| model.node(*l).map(|n| n.xyz).ok_or_else(|| Error::Invalid(format!("node {l} is missing"))))
.collect::<Result<_>>()?;
let mut mesh = Mesh { labels, xyz, elements: Vec::with_capacity(elements.len()) };
for (label, kind, nodes, formulation, d, density) in elements {
let idx: Vec<usize> = nodes.iter().filter_map(|n| mesh.node(*n)).collect();
let exyz: Vec<[f64; 3]> = idx.iter().filter_map(|i| mesh.xyz.get(*i).copied()).collect();
mesh.elements.push(Elem { label, kind, nodes: idx, xyz: exyz, formulation, d, density });
}
Ok(mesh)
}
}
/// The prescribed value of every degree of freedom (`None` = free) under a step's boundary
/// conditions. Rotational degrees of freedom do not exist on solid nodes and are ignored.
pub fn prescribed(model: &Model, resolved: &Resolved, mesh: &Mesh, step: &Step, values: bool) -> Result<Vec<Option<f64>>> {
let mut out: Vec<Option<f64>> = vec![None; mesh.dofs()];
for name in &step.boundary_conditions {
let bc = model.boundary_condition(name).ok_or_else(|| Error::Invalid(format!("boundary condition `{name}` is missing")))?;
if let Target::ReferencePoint(rp) = bc.target() {
return Err(Error::NotSupported(format!("boundary conditions on reference points (`{name}` on `{rp}`)")));
}
for &label in resolved.target_nodes(bc.target()) {
let Some(node) = mesh.node(label) else { continue };
for dof in 1..=3u8 {
let Some(v) = bc.value(dof) else { continue };
let v = if values { v } else { 0.0 };
let slot = out.get_mut(3 * node + usize::from(dof - 1)).ok_or_else(|| Error::Internal("dof index".into()))?;
match *slot {
Some(old) if old != v => {
return Err(Error::Invalid(format!(
"node {label} direction {dof} is prescribed both {old} and {v} (boundary condition `{name}` and another)"
)));
}
_ => *slot = Some(v),
}
}
}
}
Ok(out)
}
fn add(f: &mut [f64], node: usize, v: [f64; 3]) {
for (k, c) in v.iter().enumerate() {
if let Some(x) = f.get_mut(3 * node + k) {
*x += c;
}
}
}
/// The load vector of a static step: nodal forces and tractions as the model distributes them,
/// consistent pressure loads, gravity and body forces.
pub fn loads(model: &Model, resolved: &Resolved, mesh: &Mesh, step: &Step) -> Result<Vec<f64>> {
let mut f = vec![0.0; mesh.dofs()];
for name in &step.loads {
let load = model.load(name).ok_or_else(|| Error::Invalid(format!("load `{name}` is missing")))?;
match load {
Load::Force { target: Target::ReferencePoint(rp), .. } => {
return Err(Error::NotSupported(format!("loads on reference points (`{name}` on `{rp}`)")));
}
Load::Force { .. } | Load::Traction { .. } => {
for (label, v) in resolved.nodal_loads.get(name).map(Vec::as_slice).unwrap_or_default() {
let node = mesh.node(*label).ok_or_else(|| Error::Invalid(format!("load `{name}`: node {label} belongs to no solid element")))?;
add(&mut f, node, *v);
}
}
Load::Moment { .. } => {
return Err(Error::NotSupported(format!("moments (`{name}`): solid nodes have no rotations; a coupled reference point is needed")));
}
Load::Pressure { set, magnitude } => {
let faces = resolved.sets.get(set).map(|s| s.faces.as_slice()).unwrap_or_default();
for fc in faces {
let labels = model
.face_nodes(*fc)
.ok_or_else(|| Error::Invalid(format!("load `{name}`: element {} face {} is missing", fc.element, fc.face)))?;
let idx: Vec<usize> = labels
.iter()
.map(|l| mesh.node(*l).ok_or_else(|| Error::Invalid(format!("load `{name}`: node {l} belongs to no solid element"))))
.collect::<Result<_>>()?;
let xyz: Vec<[f64; 3]> = idx.iter().filter_map(|i| mesh.xyz.get(*i).copied()).collect();
let forces = face::pressure(&xyz, *magnitude).map_err(|e| Error::element(fc.element, e))?;
for (i, v) in idx.iter().zip(forces) {
add(&mut f, *i, v);
}
}
}
Load::Gravity { acceleration, set } => {
let chosen: Option<&[u32]> = set.as_ref().map(|s| resolved.sets.get(s).map(|r| r.elements.as_slice()).unwrap_or_default());
for e in &mesh.elements {
if chosen.is_some_and(|c| c.binary_search(&e.label).is_err()) {
continue;
}
let rho = e.density.ok_or_else(|| Error::Invalid(format!("load `{name}`: element {} has no density", e.label)))?;
body(&mut f, e, acceleration.map(|a| rho * a))?;
}
}
Load::BodyForce { set, vector } => {
for label in resolved.sets.get(set).map(|r| r.elements.as_slice()).unwrap_or_default() {
let e = mesh.element(*label).ok_or_else(|| Error::Invalid(format!("load `{name}`: element {label} is not a solid element")))?;
body(&mut f, e, *vector)?;
}
}
}
}
Ok(f)
}
fn body(f: &mut [f64], e: &Elem, b: [f64; 3]) -> Result<()> {
let forces = e.solid()?.body_force(b).map_err(|err| Error::element(e.label, err))?;
for (node, v) in e.nodes.iter().zip(forces) {
add(f, *node, v);
}
Ok(())
}
/// Equation numbers of the free degrees of freedom, following a node order.
pub fn equations(order: &[usize], prescribed: &[Option<f64>]) -> (Vec<Option<usize>>, usize) {
let mut map = vec![None; prescribed.len()];
let mut next = 0;
for &node in order {
for c in 0..3 {
let dof = 3 * node + c;
if prescribed.get(dof).is_some_and(Option::is_none) {
if let Some(m) = map.get_mut(dof) {
*m = Some(next);
}
next += 1;
}
}
}
(map, next)
}
+179
View File
@@ -0,0 +1,179 @@
//! Structured meshes generated in code for the analytic verification suite: a block of
//! hexahedra (hex8, hex20) or Kuhn-split tetrahedra (tet4, tet10) on [0, 1]³, mapped to the part
//! by a function, and helpers to define the model on it.
#![allow(dead_code)]
use std::collections::BTreeMap;
use modelcraft_model::{
BoundaryCondition, Elastic, ElementFace, ElementKind, Formulation, Integration, Load, Material, Model, Procedure, Section, SectionKind, Set,
Step, Symmetry, Target,
};
pub struct Grid {
pub model: Model,
/// Parametric coordinates of every node.
pub param: BTreeMap<u32, [f64; 3]>,
pub kind: ElementKind,
}
/// A structured mesh with `n` cells per direction. Nodes live on the doubled lattice
/// (2n + 1 points per direction) so quadratic elements get their mid-side nodes from the map
/// too (curved edges follow it).
pub fn grid(n: [usize; 3], kind: ElementKind, map: impl Fn([f64; 3]) -> [f64; 3]) -> Grid {
let size = n.map(|k| 2 * k + 1);
let label = |i: [usize; 3]| (1 + i[0] + size[0] * (i[1] + size[1] * i[2])) as u32;
let param_of = |i: [usize; 3]| [0, 1, 2].map(|k| i[k] as f64 / (2 * n[k]) as f64);
let mut model = Model::default();
let mut param = BTreeMap::new();
let mut node = |model: &mut Model, i: [usize; 3]| -> u32 {
let l = label(i);
if let std::collections::btree_map::Entry::Vacant(slot) = param.entry(l) {
let p = param_of(i);
model.set_node(l, map(p)).unwrap();
slot.insert(p);
}
l
};
let mut next = 1u32;
for cz in 0..n[2] {
for cy in 0..n[1] {
for cx in 0..n[0] {
let base = [2 * cx, 2 * cy, 2 * cz];
let at = |d: [usize; 3]| [base[0] + d[0], base[1] + d[1], base[2] + d[2]];
match kind {
ElementKind::Hex8 | ElementKind::Hex20 => {
let corners = [[0, 0, 0], [2, 0, 0], [2, 2, 0], [0, 2, 0], [0, 0, 2], [2, 0, 2], [2, 2, 2], [0, 2, 2]];
let mut nodes: Vec<u32> = corners.iter().map(|c| node(&mut model, at(*c))).collect();
if kind == ElementKind::Hex20 {
for e in kind.edges() {
let (a, b) = (corners[e[0]], corners[e[1]]);
nodes.push(node(&mut model, at([0, 1, 2].map(|k| (a[k] + b[k]) / 2))));
}
}
model.set_element(next, kind, nodes).unwrap();
next += 1;
}
_ => {
// Six tetrahedra around the cell's main diagonal (Kuhn), conforming across cells.
for perm in [[0, 1, 2], [0, 2, 1], [1, 0, 2], [1, 2, 0], [2, 0, 1], [2, 1, 0]] {
let mut v = [[0usize; 3]; 4];
for s in 0..3 {
v[s + 1] = v[s];
v[s + 1][perm[s]] = 2;
}
// Orientation from the parametric volume.
let p = v.map(|c| c.map(|x| x as f64));
let e = |i: usize| [0, 1, 2].map(|k| p[i][k] - p[0][k]);
let (a, b, c) = (e(1), e(2), e(3));
let vol = a[0] * (b[1] * c[2] - b[2] * c[1]) - a[1] * (b[0] * c[2] - b[2] * c[0]) + a[2] * (b[0] * c[1] - b[1] * c[0]);
if vol < 0.0 {
v.swap(1, 2);
}
let mut nodes: Vec<u32> = v.iter().map(|c| node(&mut model, at(*c))).collect();
if kind == ElementKind::Tet10 {
for e in kind.edges() {
let (a, b) = (v[e[0]], v[e[1]]);
nodes.push(node(&mut model, at([0, 1, 2].map(|k| (a[k] + b[k]) / 2))));
}
}
model.set_element(next, kind, nodes).unwrap();
next += 1;
}
}
}
}
}
}
Grid { model, param, kind }
}
pub fn near(a: f64, b: f64) -> bool {
(a - b).abs() < 1e-9
}
impl Grid {
pub fn nodes_where(&self, f: impl Fn([f64; 3]) -> bool) -> Vec<u32> {
self.param.iter().filter(|(_, p)| f(**p)).map(|(l, _)| *l).collect()
}
/// Element faces whose nodes all satisfy `f` (on parametric coordinates).
pub fn faces_where(&self, f: impl Fn([f64; 3]) -> bool) -> Vec<ElementFace> {
let mut out = Vec::new();
for (label, e) in self.model.elements() {
for (i, face) in e.kind.faces().iter().enumerate() {
if face.iter().all(|k| f(self.param[&e.nodes[*k]])) {
out.push(ElementFace { element: *label, face: i as u8 + 1 });
}
}
}
out
}
/// Material, section over every element and an empty step of the given procedure.
pub fn define(&mut self, elastic: Elastic, density: Option<f64>, formulation: Formulation, procedure: Procedure) {
let all: Vec<u32> = self.model.elements().keys().copied().collect();
self.model.add_set("all", Set { elements: all, ..Set::default() }).unwrap();
self.model.add_material("Mat", Material { elastic: Some(elastic), density }).unwrap();
self.model.add_section("solid", Section { set: "all".into(), material: "Mat".into(), kind: SectionKind::Solid {}, formulation }).unwrap();
self.model.add_step(Step::new("Step", procedure), None).unwrap();
}
pub fn node_set(&mut self, name: &str, f: impl Fn([f64; 3]) -> bool) {
let nodes = self.nodes_where(f);
self.model.add_set(name, Set { nodes, ..Set::default() }).unwrap();
}
pub fn face_set(&mut self, name: &str, f: impl Fn([f64; 3]) -> bool) {
let faces = self.faces_where(f);
self.model.add_set(name, Set { faces, ..Set::default() }).unwrap();
}
pub fn bc(&mut self, name: &str, bc: BoundaryCondition) {
self.model.add_boundary_condition(name, bc).unwrap();
self.model.set_boundary_condition_active("Step", name, true).unwrap();
}
pub fn load(&mut self, name: &str, load: Load) {
self.model.add_load(name, load).unwrap();
self.model.set_load_active("Step", name, true).unwrap();
}
pub fn symmetry(&mut self, name: &str, plane: Symmetry, f: impl Fn([f64; 3]) -> bool) {
self.node_set(name, f);
self.bc(name, BoundaryCondition::Symmetry { target: Target::Set(name.into()), plane });
}
pub fn fixed(&mut self, name: &str, f: impl Fn([f64; 3]) -> bool) {
self.node_set(name, f);
self.bc(name, BoundaryCondition::Fixed { target: Target::Set(name.into()) });
}
}
pub fn iso(young: f64, poisson: f64) -> Elastic {
Elastic::Isotropic { young, poisson }
}
pub fn full() -> Formulation {
Formulation::default()
}
pub fn reduced() -> Formulation {
Formulation { integration: Integration::Reduced, ..Formulation::default() }
}
pub fn incompatible() -> Formulation {
Formulation { incompatible_modes: true, ..Formulation::default() }
}
/// The element kinds and formulations under test.
pub fn variants() -> Vec<(ElementKind, Formulation, &'static str)> {
vec![
(ElementKind::Tet4, full(), "tet4"),
(ElementKind::Tet10, full(), "tet10"),
(ElementKind::Hex8, full(), "hex8"),
(ElementKind::Hex8, incompatible(), "hex8 incompatible"),
(ElementKind::Hex20, full(), "hex20"),
(ElementKind::Hex20, reduced(), "hex20 reduced"),
]
}
+367
View File
@@ -0,0 +1,367 @@
//! The analytic verification suite: every element and formulation against closed-form
//! solutions. Run with `--nocapture` to see the errors.
mod common;
use std::f64::consts::PI;
use common::*;
use modelcraft_model::{BoundaryCondition, ElementKind, Load, Procedure, Symmetry, Target};
use modelcraft_solver::{FrequencyOptions, Limits, MassKind, StaticResult, solve_frequency, solve_static};
fn static_solve(g: &Grid) -> StaticResult {
solve_static(&g.model, Some("Step"), &Limits::default()).unwrap()
}
fn at(r: &StaticResult, label: u32) -> usize {
r.nodes.binary_search(&label).unwrap()
}
/// Displacement patch test (MacNeal & Harder 1985 style, on a distorted 2 × 2 × 2 patch): a
/// linear displacement prescribed on the boundary is reproduced exactly inside, with exactly
/// constant strain and stress in every element.
#[test]
fn patch_test_every_element() {
let a = [[1e-3, 2e-4, -3e-4], [5e-4, -2e-3, 1e-4], [-1e-4, 3e-4, 7e-4]];
let (young, nu) = (1000.0, 0.25);
let lambda = young * nu / ((1.0 + nu) * (1.0 - 2.0 * nu));
let mu = young / (2.0 * (1.0 + nu));
let strain = [a[0][0], a[1][1], a[2][2], a[0][1] + a[1][0], a[0][2] + a[2][0], a[1][2] + a[2][1]];
let tr = strain[0] + strain[1] + strain[2];
let stress = [
lambda * tr + 2.0 * mu * strain[0],
lambda * tr + 2.0 * mu * strain[1],
lambda * tr + 2.0 * mu * strain[2],
mu * strain[3],
mu * strain[4],
mu * strain[5],
];
let field = |x: [f64; 3]| [0, 1, 2].map(|i| (0..3).map(|j| a[i][j] * x[j]).sum::<f64>());
// Interior distortion that leaves the cube's boundary in place.
let map = |p: [f64; 3]| {
let b = (PI * p[0]).sin() * (PI * p[1]).sin() * (PI * p[2]).sin();
[p[0] + 0.12 * b, p[1] - 0.08 * b, p[2] + 0.1 * b]
};
for (kind, formulation, name) in variants() {
let mut g = grid([2, 2, 2], kind, map);
g.define(iso(young, nu), None, formulation, Procedure::Static {});
let on_boundary = |p: [f64; 3]| p.iter().any(|c| near(*c, 0.0) || near(*c, 1.0));
for (i, label) in g.nodes_where(on_boundary).into_iter().enumerate() {
let x = g.model.node(label).unwrap().xyz;
let u = field(x);
let set = format!("b{i}");
g.model.add_set(&set, modelcraft_model::Set { nodes: vec![label], ..Default::default() }).unwrap();
g.bc(
&set,
BoundaryCondition::Displacement { target: Target::Set(set.clone()), values: [Some(u[0]), Some(u[1]), Some(u[2]), None, None, None] },
);
}
let r = static_solve(&g);
let mut worst: f64 = 0.0;
for (label, u) in r.nodes.iter().zip(&r.displacement) {
let want = field(g.model.node(*label).unwrap().xyz);
worst = worst.max((0..3).map(|k| (u[k] - want[k]).abs()).fold(0.0, f64::max));
}
let mut worst_stress: f64 = 0.0;
for e in &r.elements {
for p in &e.points {
worst_stress = worst_stress.max((0..6).map(|k| (p.stress[k] - stress[k]).abs()).fold(0.0, f64::max));
}
}
for s in &r.stress {
worst_stress = worst_stress.max((0..6).map(|k| (s[k] - stress[k]).abs()).fold(0.0, f64::max));
}
eprintln!("patch {name}: displacement error {worst:.1e}, stress error {worst_stress:.1e}");
assert!(worst < 1e-12, "{name}: {worst}");
assert!(worst_stress < 1e-10, "{name}: {worst_stress}");
}
}
/// Uniaxial tension by a consistent surface load on a distorted block with symmetry planes:
/// σxx = p exactly, ux = p L / E, the lateral contraction −ν p y / E, and the reactions balance
/// the load (the force form of the patch test, and a check of pressure loads).
#[test]
fn uniaxial_tension_by_pressure() {
let (young, nu, p) = (2000.0, 0.3, 5.0);
let (lx, ly, lz) = (3.0, 2.0, 1.5);
for (kind, formulation, name) in variants() {
let mut g = grid([2, 2, 2], kind, |q| {
let b = (PI * q[0]).sin() * (PI * q[1]).sin() * (PI * q[2]).sin();
[lx * q[0] + 0.2 * b, ly * q[1] + 0.1 * b, lz * q[2] - 0.1 * b]
});
g.define(iso(young, nu), None, formulation, Procedure::Static {});
g.symmetry("x0", Symmetry::X, |q| near(q[0], 0.0));
g.symmetry("y0", Symmetry::Y, |q| near(q[1], 0.0));
g.symmetry("z0", Symmetry::Z, |q| near(q[2], 0.0));
g.face_set("end", |q| near(q[0], 1.0));
// A negative pressure pulls.
g.load("pull", Load::Pressure { set: "end".into(), magnitude: -p });
let r = static_solve(&g);
let mut worst: f64 = 0.0;
for (label, u) in r.nodes.iter().zip(&r.displacement) {
let x = g.model.node(*label).unwrap().xyz;
let want = [p * x[0] / young, -nu * p * x[1] / young, -nu * p * x[2] / young];
worst = worst.max((0..3).map(|k| (u[k] - want[k]).abs()).fold(0.0, f64::max));
}
let s_err = r.stress.iter().map(|s| (s[0] - p).abs().max(s[1].abs()).max(s[5].abs())).fold(0.0, f64::max);
eprintln!("tension {name}: displacement error {worst:.1e}, stress error {s_err:.1e}");
assert!(worst < 1e-11, "{name}: {worst}");
assert!(s_err < 1e-9, "{name}: {s_err}");
assert!((r.applied_total[0] - p * ly * lz).abs() < 1e-9 && (r.reaction_total[0] + p * ly * lz).abs() < 1e-9, "{name}");
assert!(r.von_mises.iter().all(|v| (v - p).abs() < 1e-9));
}
}
/// Gravity is ρ g V, held by the reactions.
#[test]
fn gravity_and_body_force_totals() {
let mut g = grid([3, 2, 2], ElementKind::Hex20, |q| [4.0 * q[0], 2.0 * q[1], q[2]]);
g.define(iso(1000.0, 0.3), Some(2.5), full(), Procedure::Static {});
g.fixed("base", |q| near(q[2], 0.0));
g.load("g", Load::Gravity { acceleration: [0.0, 0.0, -9.81], set: None });
g.load("b", Load::BodyForce { set: "all".into(), vector: [1.0, 0.0, 0.0] });
let r = static_solve(&g);
let v = 8.0;
assert!((r.applied_total[2] + 2.5 * 9.81 * v).abs() < 1e-9, "{:?}", r.applied_total);
assert!((r.applied_total[0] - v).abs() < 1e-9);
for k in 0..3 {
assert!((r.applied_total[k] + r.reaction_total[k]).abs() < 1e-8, "{k}");
}
}
/// Cantilever L × b × h, clamped at x = 0, a shear traction on the free end. Timoshenko
/// deflection δ = P L³ / (3 E I) + P L / (κ G A), κ = 5/6, with ν = 0 so the clamp adds no
/// lateral restraint.
fn cantilever_tip(kind: ElementKind, formulation: modelcraft_model::Formulation, n: [usize; 3]) -> f64 {
let (l, b, h, young, p) = (10.0, 1.0, 1.0, 1000.0, 1.0);
let mut g = grid(n, kind, |q| [l * q[0], b * q[1], h * q[2]]);
g.define(iso(young, 0.0), None, formulation, Procedure::Static {});
g.fixed("root", |q| near(q[0], 0.0));
g.face_set("end", |q| near(q[0], 1.0));
g.load("shear", Load::Traction { set: "end".into(), vector: [0.0, 0.0, -p / (b * h)] });
let r = static_solve(&g);
let end = g.nodes_where(|q| near(q[0], 1.0));
-end.iter().map(|l| r.displacement[at(&r, *l)][2]).sum::<f64>() / end.len() as f64
}
fn timoshenko() -> f64 {
let (l, b, h, young, p) = (10.0f64, 1.0f64, 1.0f64, 1000.0, 1.0);
let i = b * h.powi(3) / 12.0;
p * l.powi(3) / (3.0 * young * i) + p * l / (5.0 / 6.0 * young / 2.0 * b * h)
}
#[test]
fn cantilever_tip_deflection_and_convergence() {
let exact = timoshenko();
let euler_bernoulli = 4.0;
eprintln!("cantilever: Timoshenko {exact:.5}, Euler–Bernoulli {euler_bernoulli:.5}");
let err = |d: f64| (d - exact).abs() / exact;
let study = |kind, f, meshes: &[[usize; 3]], name: &str| -> Vec<f64> {
meshes
.iter()
.map(|n| {
let d = cantilever_tip(kind, f, *n);
eprintln!(" {name} {n:?}: {d:.5} (error {:.2}%)", 100.0 * err(d));
err(d)
})
.collect()
};
// Quadratic and enhanced elements are accurate on coarse meshes.
let hex20 = study(ElementKind::Hex20, full(), &[[10, 1, 1], [20, 2, 2]], "hex20");
assert!(hex20[1] < 0.01);
let hex20r = study(ElementKind::Hex20, reduced(), &[[10, 2, 2]], "hex20 reduced");
assert!(hex20r[0] < 0.01);
let im = study(ElementKind::Hex8, incompatible(), &[[10, 1, 1], [20, 2, 2]], "hex8 incompatible");
assert!(im[0] < 0.03 && im[1] < 0.015);
let tet10 = study(ElementKind::Tet10, full(), &[[10, 2, 2]], "tet10");
assert!(tet10[0] < 0.02);
// Linear elements lock in bending and converge under refinement.
let meshes = [[5, 1, 1], [10, 2, 2], [20, 4, 4], [40, 8, 8]];
let hex8 = study(ElementKind::Hex8, full(), &meshes, "hex8");
let tet4 = study(ElementKind::Tet4, full(), &meshes, "tet4");
for (name, e) in [("hex8", &hex8), ("tet4", &tet4)] {
let rates: Vec<f64> = e.windows(2).map(|w| (w[0] / w[1]).log2()).collect();
eprintln!(" {name} convergence rates {rates:.2?}");
assert!(e.windows(2).all(|w| w[1] < w[0]), "{name} converges monotonically");
assert!(*rates.last().unwrap() > 1.5, "{name} approaches second order: {rates:?}");
}
assert!(hex8[3] < 0.04 && tet4[3] < 0.12, "{hex8:?} {tet4:?}");
}
/// Lamé's thick cylinder under internal pressure, plane strain (u_z = 0 on both ends), quarter
/// model: σ_r = A − B/r², σ_θ = A + B/r², A = p a²/(b² − a²), B = p a² b²/(b² − a²),
/// u_r = (1 + ν)/E ((1 − 2ν) A r + B / r).
#[test]
fn lame_thick_cylinder() {
let (a, b, t, p, young, nu) = (1.0f64, 2.0f64, 0.25, 10.0, 1000.0, 0.3);
let big_a = p * a * a / (b * b - a * a);
let big_b = p * a * a * b * b / (b * b - a * a);
let ur = |r: f64| (1.0 + nu) / young * ((1.0 - 2.0 * nu) * big_a * r + big_b / r);
let sigma_t = |r: f64| big_a + big_b / (r * r);
for (kind, formulation, n, tol_u, tol_s, name) in [
(ElementKind::Hex20, full(), [6, 8, 1], 0.002, 0.01, "hex20"),
(ElementKind::Hex8, incompatible(), [12, 16, 1], 0.01, 0.04, "hex8 incompatible"),
(ElementKind::Tet10, full(), [6, 8, 1], 0.005, 0.03, "tet10"),
] {
let mut g = grid(n, kind, |q| {
let (r, th) = (a + (b - a) * q[0], PI / 2.0 * q[1]);
[r * th.cos(), r * th.sin(), t * q[2]]
});
g.define(iso(young, nu), None, formulation, Procedure::Static {});
g.symmetry("y0", Symmetry::Y, |q| near(q[1], 0.0));
g.symmetry("x0", Symmetry::X, |q| near(q[1], 1.0));
g.node_set("ends", |q| near(q[2], 0.0) || near(q[2], 1.0));
g.bc("ends", BoundaryCondition::Symmetry { target: Target::Set("ends".into()), plane: Symmetry::Z });
g.face_set("bore", |q| near(q[0], 0.0));
g.load("p", Load::Pressure { set: "bore".into(), magnitude: p });
let r = static_solve(&g);
let mut eu: f64 = 0.0;
for (label, u) in r.nodes.iter().zip(&r.displacement) {
let x = g.model.node(*label).unwrap().xyz;
let rad = x[0].hypot(x[1]);
let got = (u[0] * x[0] + u[1] * x[1]) / rad;
eu = eu.max((got - ur(rad)).abs() / ur(a));
}
// Hoop stress at the bore (nodal average), on the 45° line to stay away from the
// symmetry edges.
let bore: Vec<u32> = g.nodes_where(|q| near(q[0], 0.0) && near(q[1], 0.5));
let st: f64 = bore
.iter()
.map(|l| {
let s = r.stress[at(&r, *l)];
let x = g.model.node(*l).unwrap().xyz;
let (c, sn) = (x[0] / x[0].hypot(x[1]), x[1] / x[0].hypot(x[1]));
// σ_θ = s_xx sin² − 2 s_xy sin cos + s_yy cos².
s[0] * sn * sn - 2.0 * s[3] * sn * c + s[1] * c * c
})
.sum::<f64>()
/ bore.len() as f64;
let es = (st - sigma_t(a)).abs() / sigma_t(a);
eprintln!("lamé {name} {n:?}: u_r error {:.3}%, bore hoop stress {st:.4} vs {:.4} ({:.2}%)", 100.0 * eu, sigma_t(a), 100.0 * es);
assert!(eu < tol_u && es < tol_s, "{name}");
}
}
/// Kirsch: a plate with a hole of radius a under remote tension σ₀, plane stress, quarter model
/// with the plate's half-width 20a. The hoop stress at the top of the hole tends to 3σ₀ (the
/// finite width adds well under 1%).
#[test]
fn kirsch_plate_with_hole() {
let (a, w, s0) = (1.0f64, 20.0f64, 1.0);
let ratio: f64 = 40.0;
let map = |q: [f64; 3]| {
let th = PI / 2.0 * q[1];
let outer = if th <= PI / 4.0 { [w, w * th.tan()] } else { [w / th.tan(), w] };
// Geometric grading toward the hole.
let s = (ratio.powf(q[0]) - 1.0) / (ratio - 1.0);
let inner = [a * th.cos(), a * th.sin()];
[inner[0] + s * (outer[0] - inner[0]), inner[1] + s * (outer[1] - inner[1]), 0.1 * q[2]]
};
let mut kt = Vec::new();
for (kind, formulation, n, name) in [
(ElementKind::Hex20, full(), [6, 8, 1], "hex20 coarse"),
(ElementKind::Hex20, full(), [12, 16, 1], "hex20 fine"),
(ElementKind::Hex8, incompatible(), [24, 32, 1], "hex8 incompatible"),
] {
let mut g = grid(n, kind, map);
g.define(iso(1000.0, 0.3), None, formulation, Procedure::Static {});
g.symmetry("x0", Symmetry::X, |q| near(q[1], 1.0));
g.symmetry("y0", Symmetry::Y, |q| near(q[1], 0.0));
g.symmetry("z0", Symmetry::Z, |q| near(q[2], 0.0));
g.face_set("right", |q| near(q[0], 1.0) && q[1] <= 0.5 + 1e-9);
g.load("pull", Load::Traction { set: "right".into(), vector: [s0, 0.0, 0.0] });
let r = static_solve(&g);
let top: Vec<u32> = g.nodes_where(|q| near(q[0], 0.0) && near(q[1], 1.0));
let k = top.iter().map(|l| r.stress[at(&r, *l)][0]).sum::<f64>() / top.len() as f64 / s0;
eprintln!("kirsch {name} {n:?}: Kt = {k:.4} (error vs 3: {:.2}%)", 100.0 * (k - 3.0).abs() / 3.0);
kt.push(k);
}
assert!((kt[1] - 3.0).abs() < (kt[0] - 3.0).abs(), "refinement approaches 3: {kt:?}");
assert!((kt[1] - 3.0).abs() / 3.0 < 0.02, "{kt:?}");
assert!((kt[2] - 3.0).abs() / 3.0 < 0.04, "{kt:?}");
}
/// Euler–Bernoulli frequencies f = (βL)² / (2π L²) √(EI/(ρA)).
fn beam_frequency(beta_l: f64, l: f64, young: f64, rho: f64, side: f64) -> f64 {
let i = side.powi(4) / 12.0;
let area = side * side;
beta_l * beta_l / (2.0 * PI * l * l) * (young * i / (rho * area)).sqrt()
}
fn beam(kind: ElementKind, n: [usize; 3], clamped: bool, modes: u32) -> Grid {
let l = 20.0;
let mut g = grid(n, kind, |q| [l * q[0], q[1], q[2]]);
g.define(iso(1000.0, 0.0), Some(1.0), full(), Procedure::Frequency { modes, min_hz: None, max_hz: None });
if clamped {
g.fixed("root", |q| near(q[0], 0.0));
}
g
}
#[test]
fn cantilever_natural_frequencies() {
let f1 = beam_frequency(1.875_104_07, 20.0, 1000.0, 1.0, 1.0);
let f2 = beam_frequency(4.694_091_13, 20.0, 1000.0, 1.0, 1.0);
for (kind, n, mass, name) in [
(ElementKind::Hex20, [20, 1, 1], MassKind::Consistent, "hex20"),
(ElementKind::Hex20, [20, 1, 1], MassKind::Lumped, "hex20 lumped"),
(ElementKind::Tet10, [20, 2, 2], MassKind::Consistent, "tet10"),
] {
let g = beam(kind, n, true, 4);
let r = solve_frequency(&g.model, Some("Step"), &FrequencyOptions { mass, shift: None }, &Limits::default()).unwrap();
let f: Vec<f64> = r.modes.iter().map(|m| m.frequency).collect();
eprintln!("cantilever modes {name}: {f:.6?} vs EB {f1:.6}, {f2:.6} ({} Lanczos vectors)", r.stats.lanczos_vectors);
assert_eq!(f.len(), 4);
// The square section bends alike in y and z: two pairs.
for (got, want, tol) in [(f[0], f1, 0.01), (f[1], f1, 0.01), (f[2], f2, 0.03), (f[3], f2, 0.03)] {
assert!((got - want).abs() / want < tol, "{name}: {got} vs {want}");
}
assert!((r.total_mass - 20.0).abs() < 1e-9);
}
}
#[test]
fn free_free_beam_has_six_rigid_body_modes() {
let g = beam(ElementKind::Hex20, [20, 1, 1], false, 8);
let r = solve_frequency(&g.model, Some("Step"), &FrequencyOptions::default(), &Limits::default()).unwrap();
let f: Vec<f64> = r.modes.iter().map(|m| m.frequency).collect();
let f1 = beam_frequency(4.730_040_74, 20.0, 1000.0, 1.0, 1.0);
eprintln!("free-free modes: {f:.6?} vs EB {f1:.6}");
assert_eq!(f.len(), 8);
assert!(f[..6].iter().all(|x| *x < 1e-3 * f1), "{f:?}");
assert!(f[6..].iter().all(|x| (x - f1).abs() / f1 < 0.015), "{f:?}");
// The rigid translations carry the whole mass as effective mass.
for d in 0..3 {
let m: f64 = r.modes[..6].iter().map(|m| m.effective_mass[d]).sum();
assert!((m - 20.0).abs() < 1e-6 * 20.0, "direction {d}: {m}");
}
assert!(r.warnings.iter().any(|w| w.contains("rigid-body")));
}
#[test]
fn results_are_deterministic() {
let g = beam(ElementKind::Tet10, [6, 1, 1], true, 3);
let a = solve_frequency(&g.model, Some("Step"), &FrequencyOptions::default(), &Limits::default()).unwrap();
let b = solve_frequency(&g.model, Some("Step"), &FrequencyOptions::default(), &Limits::default()).unwrap();
assert_eq!(a, b);
}
#[test]
fn errors_name_the_problem() {
// No boundary condition in a static step: singular, naming a node.
let mut g = grid([2, 1, 1], ElementKind::Hex8, |q| q);
g.define(iso(1000.0, 0.3), None, full(), Procedure::Static {});
g.face_set("end", |q| near(q[0], 1.0));
g.load("p", Load::Pressure { set: "end".into(), magnitude: 1.0 });
let e = solve_static(&g.model, Some("Step"), &Limits::default()).unwrap_err().to_string();
assert!(e.contains("singular at node"), "{e}");
// Caps.
g.fixed("root", |q| near(q[0], 0.0));
let tight = Limits { max_dofs: 10, ..Limits::default() };
assert!(solve_static(&g.model, Some("Step"), &tight).unwrap_err().to_string().contains("limit"));
let tight = Limits { max_factor_entries: 5, ..Limits::default() };
assert!(solve_static(&g.model, Some("Step"), &tight).unwrap_err().to_string().contains("limit"));
assert!(solve_static(&g.model, Some("Nope"), &Limits::default()).is_err());
assert!(solve_frequency(&g.model, Some("Step"), &FrequencyOptions::default(), &Limits::default()).is_err(), "a static step");
assert!(solve_static(&g.model, Some("Step"), &Limits::default()).is_ok());
}