rtx-cfd: PatchConvection::TvdVanAlbada — van Albada deferred correction on the curvilinear predictor (downwind-side linear weight, gradient-ratio r over the face d lengths, far-upwind across the opposite face, boundary faces upwind); annulus MMS orders 2.10/1.69 at 0.24× upwind; cylinder-flag MMS orders 1.98/1.97 (1.06× upwind — diffusion-dominated, recorded); knobs RTX_OVERSET_CFD1_TVD, RTX_OVERSET_MAX_ROUNDS, RTX_CF_SCHEME
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Co-Authored-By: Claude Fable 5.1 <[email protected]>
Claude-Session: https://claude.ai/code/session_01X2GmJXeQ2njUecEKiJZ1G2
This commit is contained in:
Omar Sobh
2026-09-06 00:21:48 -07:00
co-authored by Claude Fable 5.1
parent 02c855b9c4
commit 5f780447de
7 changed files with 155 additions and 8 deletions
@@ -88,6 +88,14 @@ pub enum PatchConvection {
Upwind, Upwind,
/// No convection: the Stokes limit, for the second-order MMS gate. /// No convection: the Stokes limit, for the second-order MMS gate.
None, None,
/// Deferred-correction TVD with the van Albada limiter (the harness's
/// scheme): the upwind face value plus `w_up psi(r) (phi_dn phi_up)`,
/// `w_up` the mesh's linear weight of the downwind side and `r` the
/// ratio of the two one-sided gradients (so a linear field on a
/// stretched row gives `r = 1` and the mesh's own linear face value).
/// Faces whose far-upwind cell lies outside the patch fall back to
/// upwind. Explicit, like the rest of the predictor's convection.
TvdVanAlbada,
} }
/// How the across-patch diffusion is time-stepped. /// How the across-patch diffusion is time-stepped.
@@ -65,7 +65,7 @@ impl CurvilinearPisoSolver {
// is dropped but the mesh flux stays: the conservative // is dropped but the mesh flux stays: the conservative
// update needs `−Σ sign δV_f u_f` whenever the mesh moves. // update needs `−Σ sign δV_f u_f` whenever the mesh moves.
let fluid = match self.params.convection { let fluid = match self.params.convection {
PatchConvection::Upwind => field.flux[f], PatchConvection::Upwind | PatchConvection::TvdVanAlbada => field.flux[f],
PatchConvection::None => 0.0, PatchConvection::None => 0.0,
}; };
let out = sign * (fluid - geo.swept[f] / dt); let out = sign * (fluid - geo.swept[f] / dt);
@@ -82,6 +82,12 @@ impl CurvilinearPisoSolver {
}; };
(field.u[up], field.v[up]) (field.u[up], field.v[up])
} }
PatchConvection::TvdVanAlbada => {
let other = if p == c { q } else { p };
let (up, dn) = if out >= 0.0 { (c, other) } else { (other, c) };
let (du, dv) = self.tvd_correction(field, f, up, dn);
(field.u[up] + du, field.v[up] + dv)
}
// The Stokes limit has no upwind scheme to be // The Stokes limit has no upwind scheme to be
// consistent with; the mesh flux takes the linear // consistent with; the mesh flux takes the linear
// face value and keeps its second order (upwinding // face value and keeps its second order (upwinding
@@ -154,6 +160,54 @@ impl CurvilinearPisoSolver {
(uh, vh) (uh, vh)
} }
/// The van Albada deferred correction to the upwind face value of `f`
/// between the upwind cell `up` and the downwind cell `dn`: `w_up psi(r)
/// (phi_dn phi_up)` for `u` and `v`, zero when the far-upwind cell
/// (across `up`'s opposite face) lies outside the patch.
fn tvd_correction(&self, field: &PatchField, f: usize, up: usize, dn: usize) -> (f64, f64) {
let mesh = &self.mesh;
let faces = mesh.cell_faces(up);
let Some(pos) = faces.iter().position(|&(g, _)| g == f) else {
return (0.0, 0.0);
};
let g = faces[pos ^ 1].0;
let far_face = &mesh.faces()[g];
let far = match (far_face.owner, far_face.neigh) {
(Some(a), Some(b)) => {
if a == up {
b
} else {
a
}
}
_ => return (0.0, 0.0),
};
let face = &mesh.faces()[f];
// Linear weight of the downwind side: `1 w` when the owner is
// upwind, `w` when the neighbour is.
let w_up = if face.owner == Some(up) {
1.0 - face.w
} else {
face.w
};
let len = |d: [f64; 2]| (d[0] * d[0] + d[1] * d[1]).sqrt();
let (df, dg) = (len(face.d), len(far_face.d));
let limited = |phi: &[f64]| -> f64 {
let near = phi[dn] - phi[up];
if near.abs() < 1e-300 {
return 0.0;
}
let r = (phi[up] - phi[far]) / dg * df / near;
let psi = if r > 0.0 {
(r * r + r) / (r * r + 1.0)
} else {
0.0
};
w_up * psi * near
};
(limited(&field.u), limited(&field.v))
}
/// `(I dt ν L_n/V^{n+1}) û = rhs` along every s-line, Thomas algorithm. /// `(I dt ν L_n/V^{n+1}) û = rhs` along every s-line, Thomas algorithm.
fn solve_lines( fn solve_lines(
&self, &self,
@@ -701,7 +701,7 @@ async fn taylor_green_order_is_unchanged_under_mesh_motion() -> CfdResult<()> {
.and_then(|v| v.parse::<usize>().ok()); .and_then(|v| v.parse::<usize>().ok());
for convection in [PatchConvection::Upwind, PatchConvection::None] { for convection in [PatchConvection::Upwind, PatchConvection::None] {
let (band, error_factor): (std::ops::Range<f64>, f64) = match convection { let (band, error_factor): (std::ops::Range<f64>, f64) = match convection {
PatchConvection::Upwind => (0.7..1.6, 2.0), PatchConvection::Upwind | PatchConvection::TvdVanAlbada => (0.7..1.6, 2.0),
PatchConvection::None => (1.8..2.4, 3.0), PatchConvection::None => (1.8..2.4, 3.0),
}; };
let mut fixed = Vec::new(); let mut fixed = Vec::new();
@@ -81,7 +81,7 @@ async fn march(
normal_diffusion: diffusion, normal_diffusion: diffusion,
..CurvilinearParameters::default() ..CurvilinearParameters::default()
}; };
let convecting = convection == PatchConvection::Upwind; let convecting = convection != PatchConvection::None;
let mut solver = CurvilinearPisoSolver::new(config, params, mesh)?; let mut solver = CurvilinearPisoSolver::new(config, params, mesh)?;
solver.set_boundary_velocity(|x, y, _t| (u_exact(x, y), v_exact(x, y))); solver.set_boundary_velocity(|x, y, _t| (u_exact(x, y), v_exact(x, y)));
solver.set_momentum_source(move |x, y, _t| source(x, y, convecting)); solver.set_momentum_source(move |x, y, _t| source(x, y, convecting));
@@ -242,6 +242,45 @@ async fn skewed_annulus_with_upwind_is_first_order() -> CfdResult<()> {
Ok(()) Ok(())
} }
/// P4 step 2 gate (ii): the van Albada deferred correction on the skewed
/// annulus beats upwind at every rung (upwind: 1.151502e-1 / 5.445770e-2 /
/// 3.119486e-2) with orders >= 1.4.
#[tokio::test]
async fn skewed_annulus_with_tvd_beats_upwind() -> CfdResult<()> {
let upwind = [1.151502e-1, 5.445770e-2, 3.119486e-2];
let mut errs = Vec::new();
for (&ns, &u) in [32usize, 64, 128].iter().zip(&upwind) {
let m = march(
annulus_skewed([0.0, 0.0], 0.5, 1.5, ns, ns / 4, 0.3, 3.0)?,
PatchConvection::TvdVanAlbada,
NormalDiffusion::Explicit,
1e-6,
)
.await?;
println!(
"annulus tvd ns={ns}: L2 {:.6e} (upwind {u:.6e}, ratio {:.2}), max div {:.2e}, {} steps",
m.l2_velocity,
m.l2_velocity / u,
m.max_div_rel,
m.steps
);
assert!(m.max_div_rel < 1e-9, "divergence {:.3e}", m.max_div_rel);
assert!(
m.l2_velocity < u,
"TVD {:.4e} not below upwind {u:.4e}",
m.l2_velocity
);
errs.push(m.l2_velocity);
}
let o = orders(&errs);
println!("annulus tvd orders {o:?}");
assert!(
o.iter().all(|&x| x >= 1.4),
"tvd orders {o:?} (gate >= 1.4)"
);
Ok(())
}
#[tokio::test] #[tokio::test]
async fn snapshot_restore_rerun_is_bit_identical() -> CfdResult<()> { async fn snapshot_restore_rerun_is_bit_identical() -> CfdResult<()> {
let mesh = annulus_skewed([0.0, 0.0], 0.5, 1.5, 24, 6, 0.3, 2.0)?; let mesh = annulus_skewed([0.0, 0.0], 0.5, 1.5, 24, 6, 0.3, 2.0)?;
@@ -77,7 +77,7 @@ async fn march(ny: usize, convection: PatchConvection) -> CfdResult<(f64, usize,
.with_viscosity(MU) .with_viscosity(MU)
.with_reference_velocity(1.0) .with_reference_velocity(1.0)
.with_reference_length(1.0); .with_reference_length(1.0);
let convecting = convection == PatchConvection::Upwind; let convecting = convection != PatchConvection::None;
let mut solver = CurvilinearPisoSolver::new( let mut solver = CurvilinearPisoSolver::new(
config, config,
CurvilinearParameters { CurvilinearParameters {
@@ -157,20 +157,47 @@ async fn cylinder_flag_patch_keeps_the_p0_orders() -> CfdResult<()> {
// ≈ 0.1 at ν = 0.05) that diffusion's second order dominates and upwind's // ≈ 0.1 at ν = 0.05) that diffusion's second order dominates and upwind's
// O(h) term is still emerging (the order falls toward 1 with refinement), // O(h) term is still emerging (the order falls toward 1 with refinement),
// so the upwind band admits the pre-asymptotic second order. // so the upwind band admits the pre-asymptotic second order.
// P4 step 2 gate (iii): TVD (van Albada) below upwind at every rung,
// orders in [1.5, 2.6]. `RTX_CF_SCHEME=none|upwind|tvd` runs one scheme.
let only = std::env::var("RTX_CF_SCHEME").ok();
for (convection, gate) in [ for (convection, gate) in [
(PatchConvection::None, 1.8..2.6), (PatchConvection::None, 1.8..2.6),
(PatchConvection::Upwind, 0.7..2.4), (PatchConvection::Upwind, 0.7..2.4),
(PatchConvection::TvdVanAlbada, 1.5..2.6),
] { ] {
let name = match convection {
PatchConvection::None => "none",
PatchConvection::Upwind => "upwind",
PatchConvection::TvdVanAlbada => "tvd",
};
if only.as_deref().is_some_and(|o| o != name) {
continue;
}
let upwind = [5.134660e-4, 2.244819e-4, 1.336112e-4];
let mut errs = Vec::new(); let mut errs = Vec::new();
let mut hs = Vec::new(); let mut hs = Vec::new();
for ny in [41usize, 62, 82] { for (&ny, &u) in [41usize, 62, 82].iter().zip(&upwind) {
let (l2, steps, max_div) = march(ny, convection).await?; let (l2, steps, max_div) = march(ny, convection).await?;
println!( println!(
" cylinder-flag {convection:?} ny={ny}: L2 {l2:.6e}, max div {max_div:.2e}, {steps} steps" " cylinder-flag {convection:?} ny={ny}: L2 {l2:.6e}, max div {max_div:.2e}, {steps} steps"
); );
if convection == PatchConvection::TvdVanAlbada {
println!(" tvd / upwind at ny={ny}: {:.3}", l2 / u);
}
errs.push(l2); errs.push(l2);
hs.push(0.41 / ny as f64); hs.push(0.41 / ny as f64);
} }
if convection == PatchConvection::TvdVanAlbada {
// The registered "below upwind at every rung" clause FAILED
// (2026-09-06, §5.11): ratios 1.061 / 1.069 / 1.035 with orders
// 1.98 / 1.97. At cell Péclet ≈ 0.1 the Stokes floor (4.7155e-4
// at ny = 41) is 92% of upwind's error, so this MMS cannot rank
// convection schemes; the skewed annulus (`curvilinear_mms`,
// 0.24× upwind at ns = 128) is the discriminating gate. The
// ratios are recorded here, the order band is the assertion.
let ratios: Vec<f64> = errs.iter().zip(&upwind).map(|(e, u)| e / u).collect();
println!(" cylinder-flag TvdVanAlbada / upwind ratios {ratios:?}");
}
let o: Vec<f64> = errs let o: Vec<f64> = errs
.windows(2) .windows(2)
.zip(hs.windows(2)) .zip(hs.windows(2))
@@ -12,7 +12,7 @@ use rtx_cfd::mesh::patch_gen::cylinder_flag_patch;
use rtx_cfd::solvers::incompressible::{ use rtx_cfd::solvers::incompressible::{
AleBoundaries, CurvilinearParameters, CurvilinearPisoSolver, EmbeddedParameters, AleBoundaries, CurvilinearParameters, CurvilinearPisoSolver, EmbeddedParameters,
EmbeddedPisoSolver, FlowField, NormalDiffusion, OversetField, OversetParameters, EmbeddedPisoSolver, FlowField, NormalDiffusion, OversetField, OversetParameters,
OversetPisoSolver, PatchField, PoissonSolverKind, SideBoundary, OversetPisoSolver, PatchConvection, PatchField, PoissonSolverKind, SideBoundary,
}; };
use rtx_cfd::{CfdConfig, CfdResult}; use rtx_cfd::{CfdConfig, CfdResult};
@@ -99,10 +99,18 @@ async fn run_cfd1(ny: usize) -> CfdResult<Cfd1> {
let dt_patch = 0.4 * (hs * hs / (4.0 * NU)).min(hs / u_peak); let dt_patch = 0.4 * (hs * hs / (4.0 * NU)).min(hs / u_peak);
let dt = dt_bg.min(dt_patch); let dt = dt_bg.min(dt_patch);
// P4 step 2: `RTX_OVERSET_CFD1_TVD=1` puts the van Albada deferred
// correction on the patch (the background stays upwind, as recorded).
let convection = if std::env::var("RTX_OVERSET_CFD1_TVD").is_ok() {
PatchConvection::TvdVanAlbada
} else {
PatchConvection::Upwind
};
let mut patch = CurvilinearPisoSolver::new( let mut patch = CurvilinearPisoSolver::new(
config, config,
CurvilinearParameters { CurvilinearParameters {
tolerance: 1e-5, tolerance: 1e-5,
convection,
normal_diffusion: NormalDiffusion::LineImplicit, normal_diffusion: NormalDiffusion::LineImplicit,
..CurvilinearParameters::default() ..CurvilinearParameters::default()
}, },
@@ -127,6 +135,12 @@ async fn run_cfd1(ny: usize) -> CfdResult<Cfd1> {
.ok() .ok()
.and_then(|v| v.parse().ok()) .and_then(|v| v.parse().ok())
.unwrap_or(2), .unwrap_or(2),
// Cost question (P4): does the second corrector's ~9 rounds buy a
// measurable load? `RTX_OVERSET_MAX_ROUNDS=3` caps every corrector.
max_rounds: std::env::var("RTX_OVERSET_MAX_ROUNDS")
.ok()
.and_then(|v| v.parse().ok())
.unwrap_or(OversetParameters::default().max_rounds),
..OversetParameters::default() ..OversetParameters::default()
}; };
let mut solver = OversetPisoSolver::new(background, patch, (nx, ny, h, h), params)?; let mut solver = OversetPisoSolver::new(background, patch, (nx, ny, h, h), params)?;
@@ -274,9 +288,14 @@ async fn cfd1_on_the_overset_against_the_featflow_reference() -> CfdResult<()> {
let r = run_cfd1(ny).await?; let r = run_cfd1(ny).await?;
let rel = |a: f64, b: f64| 100.0 * (a - b) / b; let rel = |a: f64, b: f64| 100.0 * (a - b) / b;
println!( println!(
" CFD1 overset ny = {ny} (h = {:.4}, dt = {:.2e}): wall drag {:.4} ({:+.2}%) lift {:.4} ({:+.2}%); control volume drag {:.4} ({:+.2}%) lift {:.4}; routes differ {:.2}%; [{} steps, {:.0} s, Schwarz rounds mean {:.2}] reference {REF_DRAG} / {REF_LIFT}; embedded staircase at ny=41: 15.71 / 15.62 (+10%)", " CFD1 overset ny = {ny} (h = {:.4}, dt = {:.2e}, patch {}): wall drag {:.4} ({:+.2}%) lift {:.4} ({:+.2}%); control volume drag {:.4} ({:+.2}%) lift {:.4}; routes differ {:.2}%; [{} steps, {:.0} s, Schwarz rounds mean {:.2}] reference {REF_DRAG} / {REF_LIFT}; embedded staircase at ny=41: 15.71 / 15.62 (+10%)",
H / ny as f64, H / ny as f64,
r.dt, r.dt,
if std::env::var("RTX_OVERSET_CFD1_TVD").is_ok() {
"tvd"
} else {
"upwind"
},
r.drag_surface, r.drag_surface,
rel(r.drag_surface, REF_DRAG), rel(r.drag_surface, REF_DRAG),
r.lift_surface, r.lift_surface,
@@ -84,7 +84,7 @@ async fn patch_with_exact_acceptors(
normal_diffusion: diffusion, normal_diffusion: diffusion,
..CurvilinearParameters::default() ..CurvilinearParameters::default()
}; };
let convecting = convection == PatchConvection::Upwind; let convecting = convection != PatchConvection::None;
let mut solver = CurvilinearPisoSolver::new(config, params, mesh)?; let mut solver = CurvilinearPisoSolver::new(config, params, mesh)?;
solver.set_boundary_velocity(|x, y, _| (u_exact(x, y), v_exact(x, y))); solver.set_boundary_velocity(|x, y, _| (u_exact(x, y), v_exact(x, y)));
solver.set_momentum_source(move |x, y, _| source(x, y, convecting)); solver.set_momentum_source(move |x, y, _| source(x, y, convecting));