embedded3 S2-3c: the 2D solver on the flag wake's kinematics (the reference for the 3D full-span run)
CI / Python Bindings (maturin) (ubuntu-latest) (push) Blocked by required conditions
CI / WASM Build + Size Check (push) Blocked by required conditions
CI / Distributed Training Tests (push) Blocked by required conditions
CI / CI Success (push) Blocked by required conditions
CI / Build (macos-latest) (push) Waiting to run
CI / Test (macos-latest) (push) Blocked by required conditions
CI / Test (ubuntu-latest) (push) Blocked by required conditions
CI / Python Bindings (maturin) (macos-latest) (push) Blocked by required conditions
CI / Clippy Check (push) Failing after 3s
Performance Benchmarks / Run Benchmarks (push) Failing after 4s
CI / Format Check (push) Failing after 4s
CI / Build CPU-Only (Explicit) (push) Failing after 4s
Documentation / Build User Guide (push) Successful in 7s
CI / Build (ubuntu-latest) (push) Failing after 53s
Documentation / Build API Documentation (push) Failing after 54s

Co-Authored-By: Claude Fable 5.1 <[email protected]>
This commit is contained in:
Omar Sobh
2026-09-17 23:14:42 -05:00
co-authored by Claude Fable 5.1
parent 6d2872e7d0
commit f2cdda4691
@@ -0,0 +1,240 @@
//! S2-3c: the 2D solver on the flag wake's exact kinematics — the same
//! cylinder + capsule flag, the same first-mode motion (tip 84 mm at
//! 1.930 Hz), the same inflow mean (Ū 1.0, the 2D parabola), TVD, on the
//! ny 62 spacing (378 × 62, h 6.6 mm). Its loads are the 2D answer for
//! this kinematics; the 3D full-span run must reproduce them. Loads by
//! the traction sampler over the flag's and the cylinder's surface
//! samples per unit span, every 10 steps; the last period's mean drag and
//! median-filtered lift swing.
//!
//! `cargo test --release -p rtx-cfd --test embedded3_flag_reference_2d -- --ignored --nocapture`
use rtx_cfd::solvers::incompressible::{
AleBoundaries, ConvectionScheme, EmbeddedBody, EmbeddedParameters, EmbeddedPisoSolver,
FlowField, MgPrecision, MgSmoother, PoissonSolverKind, SideBoundary,
};
use rtx_cfd::{CfdConfig, CfdResult};
const H: f64 = 0.41;
const L: f64 = 2.5;
const CX: f64 = 0.2;
const CY: f64 = 0.2;
const R_CYL: f64 = 0.05;
const FLAG_X0: f64 = 0.6;
const FLAG_LEN: f64 = 0.35;
const FLAG_HALF: f64 = 0.01;
const AMP: f64 = 0.084;
const FREQ: f64 = 1.930;
const U_MEAN: f64 = 1.0;
const RHO: f64 = 1000.0;
const NU: f64 = 1e-3;
const BETA_L: f64 = 1.875_104_069;
fn mode(s: f64) -> f64 {
let b = BETA_L;
let sigma = (b.sinh() - b.sin()) / (b.cosh() + b.cos());
let phi = |s: f64| (b * s).cosh() - (b * s).cos() - sigma * ((b * s).sinh() - (b * s).sin());
phi(s) / phi(1.0)
}
fn deflection(s: f64, t: f64) -> (f64, f64) {
let w = 2.0 * std::f64::consts::PI * FREQ;
(
AMP * mode(s) * (w * t).sin(),
AMP * mode(s) * w * (w * t).cos(),
)
}
fn centreline(m: usize, n: usize, t: f64) -> (f64, f64, f64) {
let s = m as f64 / n as f64;
let (d, v) = deflection(s, t);
(FLAG_X0 + s * FLAG_LEN, CY + d, v)
}
/// Distance to the capsule flag and the centreline velocity at the foot.
fn flag_sdf(x: f64, y: f64, t: f64) -> (f64, f64) {
let n = 40;
let mut best = f64::INFINITY;
let mut v_best = 0.0;
for m in 0..n {
let (ax, ay, av) = centreline(m, n, t);
let (bx, by, bv) = centreline(m + 1, n, t);
let (ex, ey) = (bx - ax, by - ay);
let u = (((x - ax) * ex + (y - ay) * ey) / (ex * ex + ey * ey)).clamp(0.0, 1.0);
let d = ((x - ax - u * ex).powi(2) + (y - ay - u * ey).powi(2)).sqrt();
if d < best {
best = d;
v_best = av + u * (bv - av);
}
}
(best - FLAG_HALF, v_best)
}
fn cyl_sdf(x: f64, y: f64) -> f64 {
((x - CX).powi(2) + (y - CY).powi(2)).sqrt() - R_CYL
}
/// Surface samples `(x, y, nx, ny, ds)` at `t`: the flag's two sides and
/// tip along the deflected centreline, the cylinder's circle; samples
/// inside the other body are dropped.
fn samples(t: f64, ds: f64) -> Vec<(f64, f64, f64, f64, f64)> {
let mut out = Vec::new();
let n = ((FLAG_LEN / ds).ceil() as usize).max(8);
for m in 0..n {
let (ax, ay, _) = centreline(m, n, t);
let (bx, by, _) = centreline(m + 1, n, t);
let (ex, ey) = (bx - ax, by - ay);
let len = (ex * ex + ey * ey).sqrt();
let (tx, ty) = (ex / len, ey / len);
let (nx, ny) = (-ty, tx);
let (mx, my) = (0.5 * (ax + bx), 0.5 * (ay + by));
for sign in [1.0, -1.0] {
let (px, py) = (mx + sign * FLAG_HALF * nx, my + sign * FLAG_HALF * ny);
if cyl_sdf(px, py) > 0.0 {
out.push((px, py, sign * nx, sign * ny, len));
}
}
}
// The tip: a semicircle around the last centreline point.
let (tx0, ty0, _) = centreline(n, n, t);
let (px, py, _) = centreline(n - 1, n, t);
let ang0 = (ty0 - py).atan2(tx0 - px);
let n_arc = ((std::f64::consts::PI * FLAG_HALF / ds).ceil() as usize).max(4);
for k in 0..n_arc {
let a = ang0 - std::f64::consts::FRAC_PI_2
+ (k as f64 + 0.5) / n_arc as f64 * std::f64::consts::PI;
out.push((
tx0 + FLAG_HALF * a.cos(),
ty0 + FLAG_HALF * a.sin(),
a.cos(),
a.sin(),
std::f64::consts::PI * FLAG_HALF / n_arc as f64,
));
}
let n_c = ((2.0 * std::f64::consts::PI * R_CYL / ds).ceil() as usize).max(16);
for k in 0..n_c {
let a = (k as f64 + 0.5) / n_c as f64 * 2.0 * std::f64::consts::PI;
let (px, py) = (CX + R_CYL * a.cos(), CY + R_CYL * a.sin());
if flag_sdf(px, py, t).0 > 0.0 {
out.push((
px,
py,
a.cos(),
a.sin(),
2.0 * std::f64::consts::PI * R_CYL / n_c as f64,
));
}
}
out
}
fn median(v: &[f64]) -> f64 {
let mut s = v.to_vec();
s.sort_by(|a, b| a.partial_cmp(b).unwrap());
s[s.len() / 2]
}
#[tokio::test]
#[ignore = "S2-3c: the 2D reference for the flag wake's kinematics (minutes on the host)"]
async fn flag_wake_2d_reference() -> CfdResult<()> {
let ny = 62;
let h = H / ny as f64;
let nx = (L / h).round() as usize;
let dt = 8.817e-4;
let period = 1.0 / FREQ;
let t_end = 2.0 * period;
let config = CfdConfig::new()
.with_density(RHO)
.with_viscosity(RHO * NU)
.with_reference_velocity(U_MEAN)
.with_reference_length(2.0 * R_CYL);
let mut solver = EmbeddedPisoSolver::new(
config,
EmbeddedParameters {
corrector_steps: 3,
tolerance: 1e-8,
boundaries: AleBoundaries {
right: SideBoundary::PressureOutlet,
..AleBoundaries::default()
},
poisson_solver: PoissonSolverKind::Multigrid,
poisson_precision: MgPrecision::F64,
poisson_smoother: MgSmoother::Lexicographic,
convection_scheme: ConvectionScheme::TvdVanAlbada,
},
)?;
solver.set_boundary_velocity(|x, y, _t| {
if x <= 0.0 {
(1.5 * U_MEAN * y * (H - y) / (0.5 * H).powi(2), 0.0)
} else {
(0.0, 0.0)
}
});
let flag = EmbeddedBody::from_sdf(|x, y, t| flag_sdf(x, y, t).0)
.with_surface_velocity(|x, y, t| (0.0, flag_sdf(x, y, t).1));
solver.set_moving_body(EmbeddedBody::union(
EmbeddedBody::circle(CX, CY, R_CYL),
flag,
));
let mut field = FlowField::new(nx, ny, h, h)?;
for j in 0..ny {
let u0 =
1.5 * U_MEAN * ((j as f64 + 0.5) * h) * (H - (j as f64 + 0.5) * h) / (0.5 * H).powi(2);
for i in 0..=nx {
field.u[(j, i)] = u0;
}
}
solver.initialize(&mut field)?;
let steps = (t_end / dt).ceil() as usize;
println!(" 2D reference: {nx}×{ny}, h {h:.4e}, dt {dt:.3e}, {steps} steps");
let mu = RHO * NU;
let start = std::time::Instant::now();
let mut drag = Vec::new();
let mut lift = Vec::new();
let mut worst = 0.0_f64;
for step in 0..steps {
let r = solver.advance(&mut field, dt).await?;
worst = worst.max(r.solver_result.final_residual);
let t = (step + 1) as f64 * dt;
if (step + 1) % 10 == 0 {
let mask = solver.mask().expect("mask");
let body = solver.body().expect("body");
let (mut fx, mut fy, mut skipped) = (0.0, 0.0, 0usize);
for (x, y, nx_, ny_, ds) in samples(t, 0.5 * h) {
match mask.traction_at(body, &field.u, &field.v, &field.p, mu, t, x, y, nx_, ny_) {
Some((tx, ty)) => {
fx += tx * ds;
fy += ty * ds;
}
None => skipped += 1,
}
}
if t >= t_end - period {
drag.push(fx);
lift.push(fy);
}
if (step + 1) % 100 == 0 {
println!(
" t {t:6.3} tip {:+.4}: drag {fx:7.1} lift {fy:+8.1} N/m (skipped {skipped}); residual {:.1e}; [{:.0} s]",
deflection(1.0, t).0,
r.solver_result.final_residual,
start.elapsed().as_secs_f64()
);
}
}
}
let filt: Vec<f64> = (0..lift.len())
.map(|i| median(&lift[i.saturating_sub(5)..(i + 6).min(lift.len())]))
.collect();
let lo = filt.iter().cloned().fold(f64::INFINITY, f64::min);
let hi = filt.iter().cloned().fold(f64::NEG_INFINITY, f64::max);
println!(
" FINAL 2D reference: last period drag mean {:.1} N/m, lift swing {:+.1}{:+.1} (raw {:+.1}{:+.1}); worst residual {worst:.1e}; {:.0} s",
drag.iter().sum::<f64>() / drag.len() as f64,
lo,
hi,
lift.iter().cloned().fold(f64::INFINITY, f64::min),
lift.iter().cloned().fold(f64::NEG_INFINITY, f64::max),
start.elapsed().as_secs_f64()
);
Ok(())
}