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rustytorch/crates/specialized/rtx-cfd/tests/embedded3_dfg_2z.rs
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Omar SobhandClaude Fable 5.1 b34f6ad966
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embedded3 S2-1 remedy: the reconstructed wall route on the cut geometry's polygons (two probes along the interpolant normal) — sphere MMS 11.3/8.3 % (the best route); wired into the DFG and flag drivers
Co-Authored-By: Claude Fable 5.1 <[email protected]>
2026-09-17 23:18:21 -05:00

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//! embedded3 item 12: SchäferTurek DFG 3D-2Z (the laminar cylinder in the
//! square channel, Re 20, steady) on the device cut-cell wall. Channel
//! 2.5 × 0.41 × 0.41, cylinder D 0.1 at (0.5, 0.2) across the width,
//! inflow U(y, z) = 16 U_m y z (H y)(H z)/H⁴ with U_m 0.45 (Ū = 0.2),
//! ρ 1, ν 1e-3. Coefficients `c = 2F/(ρ Ū² D H)`, Δp between the front
//! and back stagnation points. Reference (the DFG bar): c_D 6.056.25,
//! c_L 0.0080.010, Δp 0.1650.175.
//!
//! `RTX_E3_DFG_NY=62 RTX_CUDA_ARCH=sm_120 cargo test --release -p rtx-cfd --features cuda --test embedded3_dfg_2z -- --ignored --nocapture`
//! `RTX_E3_DFG_T` sets the flow time marched (default 10 s); `RTX_E3_DFG_VTK=<dir>`
//! writes the final instant; `RTX_E3_DFG_CSV=<path>` the load history.
#![cfg(feature = "cuda")]
use rtx_cfd::solvers::incompressible::ConvectionScheme;
use rtx_cfd::solvers::incompressible::embedded3::step::device::DeviceStep;
use rtx_cfd::solvers::incompressible::embedded3::{
Body, Boundaries, Field, Fluid, Grid, Parameters, Side, Solver, WallScheme, write_vtk,
};
use std::io::Write as _;
const H: f64 = 0.41;
const L: f64 = 2.5;
const D: f64 = 0.1;
const CX: f64 = 0.5;
const CY: f64 = 0.2;
const U_M: f64 = 0.45;
const U_BAR: f64 = 4.0 / 9.0 * U_M;
const RHO: f64 = 1.0;
const NU: f64 = 1e-3;
fn env_f(name: &str, default: f64) -> f64 {
std::env::var(name)
.ok()
.and_then(|v| v.parse().ok())
.unwrap_or(default)
}
fn inflow(y: f64, z: f64) -> f64 {
16.0 * U_M * y * z * (H - y) * (H - z) / (H * H * H * H)
}
#[test]
#[ignore = "item 12: the DFG rung on the device (minutes at ny 62, hours at ny 123)"]
fn dfg_3d_2z_on_the_device() {
let ny = env_f("RTX_E3_DFG_NY", 62.0) as usize;
let h = H / ny as f64;
let nx = (L / h).round() as usize;
let nz = ny;
let t_end = env_f("RTX_E3_DFG_T", 10.0);
// Explicit stability: CFL 0.3 on U_m and half the viscous limit.
let dt = (0.3 * h / U_M).min(0.5 * h * h / (6.0 * NU));
let mut solver = Solver::new(
Fluid {
density: RHO,
viscosity: RHO * NU,
reference_velocity: U_BAR,
reference_length: D,
},
Parameters {
corrector_steps: 2,
tolerance: 1e-8,
convection_scheme: ConvectionScheme::TvdVanAlbada,
wall_scheme: WallScheme::CutCell,
boundaries: Boundaries {
x1: Side::PressureOutlet,
..Boundaries::default()
},
..Parameters::default()
},
);
solver.set_boundary_velocity(|x, y, z, _t| {
if x <= 0.0 {
(inflow(y, z), 0.0, 0.0)
} else {
(0.0, 0.0, 0.0)
}
});
// The cylinder extruded across the width, with samples for the
// traction route (S2-1).
solver.set_body(Body::extruded(
rtx_cfd::solvers::incompressible::EmbeddedBody::circle(CX, CY, 0.5 * D),
H,
));
let g = Grid::cubic(nx, ny, nz, h);
let mut field = Field::new(g);
// Start from the inflow profile everywhere (a faster approach to steady).
for k in 0..nz {
for j in 0..ny {
let u0 = inflow((j as f64 + 0.5) * h, (k as f64 + 0.5) * h);
for i in 0..=nx {
field.u[g.uface(k, j, i)] = u0;
}
}
}
solver.initialize(&mut field);
let mask_cells = solver.mask().map_or(0, |m| m.fluid_cells());
println!(
" DFG 3D-2Z ny {ny}: {nx}×{ny}×{nz} = {} cells ({mask_cells} fluid), h {h:.4e}, dt {dt:.3e}, t_end {t_end}",
g.cells()
);
let mut device = DeviceStep::new(solver, g);
device.upload(&field);
let steps = (t_end / dt).ceil() as usize;
let coef = 2.0 / (RHO * U_BAR * U_BAR * D * H);
let csv = std::env::var("RTX_E3_DFG_CSV").ok().map(|p| {
let mut f = std::fs::File::create(p).expect("csv");
writeln!(
f,
"t,cd_wall,cl_wall,cd_cv,cl_cv,dp,residual,cg,cd_sampler,cl_sampler"
)
.unwrap();
f
});
let mut csv = csv;
let sample_every = (steps / 100).max(1);
let start = std::time::Instant::now();
let mut last: Option<(f64, f64, f64, f64, f64)> = None;
let mut last_sampler = (f64::NAN, f64::NAN);
let mut settled = false;
for step in 0..steps {
let r = device.advance(dt);
if (step + 1) % sample_every == 0 || step + 1 == steps {
device.download(&mut field);
let solver = &device.solver;
let mask = solver.mask().expect("mask");
let body = solver.body().expect("body");
let t = solver.time();
let fw = mask
.cut_wall_force(body, &field, RHO * NU, t)
.expect("wall");
let margin = 3.0 * D;
let ci = |x: f64| ((x / h).round() as usize).clamp(2, nx - 2);
let cj = |y: f64| ((y / h).round() as usize).clamp(2, ny - 2);
let bx = (
ci(CX - margin),
ci(CX + margin),
cj(CY - 0.15),
cj(CY + 0.15),
0,
nz,
);
let fcv =
mask.control_volume_force_with_walls(&field, dt, RHO, RHO * NU, None, bx, true);
// The reconstructed wall route (two probes on the cut polygons).
let fr = mask
.cut_wall_force_reconstructed(body, &field, RHO * NU, t, None)
.expect("reconstructed");
let fs = rtx_cfd::solvers::incompressible::embedded3::SurfaceForce {
f: fr,
samples: 0,
skipped: 0,
};
let (cd_s, cl_s) = (coef * fs.f[0], coef * fs.f[1]);
let zc = 0.5 * H;
let p_front = mask
.pressure_at(&field.p, CX - 0.5 * D, CY, zc)
.unwrap_or(f64::NAN);
let p_back = mask
.pressure_at(&field.p, CX + 0.5 * D, CY, zc)
.unwrap_or(f64::NAN);
let dp = p_front - p_back;
let (cd, cl, cd_cv, cl_cv) = (coef * fw[0], coef * fw[1], coef * fcv[0], coef * fcv[1]);
println!(
" t {t:8.4}: c_D {cd:.4} (CV {cd_cv:.4}, reconstructed {cd_s:.4} skipped {}) c_L {cl:.5} (CV {cl_cv:.5}, reconstructed {cl_s:.5}) Δp {dp:.4} residual {:.1e} CG {} [{:.0} s]",
fs.skipped,
r.final_residual,
r.poisson_iterations,
start.elapsed().as_secs_f64()
);
if let Some(f) = csv.as_mut() {
writeln!(
f,
"{t:.5},{cd:.6},{cl:.6},{cd_cv:.6},{cl_cv:.6},{dp:.6},{:.3e},{},{cd_s:.6},{cl_s:.6}",
r.final_residual, r.poisson_iterations
)
.unwrap();
}
last_sampler = (cd_s, cl_s);
if let Some((pcd, pcl, _, _, pdp)) = last {
let rel = ((cd - pcd) / cd)
.abs()
.max(((dp - pdp) / dp).abs())
.max((cl - pcl).abs() / 0.01);
if rel < 1e-4 && t > 2.0 {
settled = true;
}
}
last = Some((cd, cl, cd_cv, cl_cv, dp));
if settled {
println!(" settled (relative change < 1e-4 between samples)");
break;
}
}
}
device.download(&mut field);
let solver = &device.solver;
let mask = solver.mask().expect("mask");
if let Ok(dir) = std::env::var("RTX_E3_DFG_VTK") {
let path = std::path::Path::new(&dir).join(format!("dfg_2z_ny{ny}.vtk"));
write_vtk(&path, &field, Some(mask)).expect("vtk");
println!(" instant written to {}", path.display());
}
let (cd, cl, cd_cv, cl_cv, dp) = last.expect("samples");
println!(
" FINAL ny {ny}: c_D {cd:.4} (CV {cd_cv:.4}, routes {:.2e} apart; reconstructed {:.4}, {:.2e} from CV) c_L {cl:.5} (CV {cl_cv:.5}, reconstructed {:.5}) Δp {dp:.4} — reference c_D 6.056.25, c_L 0.0080.010, Δp 0.1650.175; {:.0} s",
((cd - cd_cv) / cd).abs(),
last_sampler.0,
((last_sampler.0 - cd_cv) / cd_cv).abs(),
last_sampler.1,
start.elapsed().as_secs_f64()
);
if let Some(t) = device.timers() {
println!(" timers: {t:?}");
}
}