embedded3 item 12: the DFG 3D-2Z device driver (loads by both routes, Δp, settle criterion, CSV) and the VTK instant export
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Co-Authored-By: Claude Fable 5.1 <[email protected]>
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co-authored by
Claude Fable 5.1
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//! embedded3 item 12: Schäfer–Turek DFG 3D-2Z (the laminar cylinder in the
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//! square channel, Re 20, steady) on the device cut-cell wall. Channel
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//! 2.5 × 0.41 × 0.41, cylinder D 0.1 at (0.5, 0.2) across the width,
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//! inflow U(y, z) = 16 U_m y z (H − y)(H − z)/H⁴ with U_m 0.45 (Ū = 0.2),
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//! ρ 1, ν 1e-3. Coefficients `c = 2F/(ρ Ū² D H)`, Δp between the front
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//! and back stagnation points. Reference (the DFG bar): c_D 6.05–6.25,
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//! c_L 0.008–0.010, Δp 0.165–0.175.
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//!
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//! `RTX_E3_DFG_NY=62 RTX_CUDA_ARCH=sm_120 cargo test --release -p rtx-cfd --features cuda --test embedded3_dfg_2z -- --ignored --nocapture`
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//! `RTX_E3_DFG_T` sets the flow time marched (default 10 s); `RTX_E3_DFG_VTK=<dir>`
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//! writes the final instant; `RTX_E3_DFG_CSV=<path>` the load history.
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#![cfg(feature = "cuda")]
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use rtx_cfd::solvers::incompressible::ConvectionScheme;
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use rtx_cfd::solvers::incompressible::embedded3::step::device::DeviceStep;
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use rtx_cfd::solvers::incompressible::embedded3::{
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Body, Boundaries, Field, Fluid, Grid, Parameters, Side, Solver, WallScheme, write_vtk,
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};
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use std::io::Write as _;
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const H: f64 = 0.41;
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const L: f64 = 2.5;
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const D: f64 = 0.1;
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const CX: f64 = 0.5;
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const CY: f64 = 0.2;
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const U_M: f64 = 0.45;
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const U_BAR: f64 = 4.0 / 9.0 * U_M;
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const RHO: f64 = 1.0;
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const NU: f64 = 1e-3;
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fn env_f(name: &str, default: f64) -> f64 {
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std::env::var(name)
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.ok()
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.and_then(|v| v.parse().ok())
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.unwrap_or(default)
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}
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fn inflow(y: f64, z: f64) -> f64 {
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16.0 * U_M * y * z * (H - y) * (H - z) / (H * H * H * H)
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}
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#[test]
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#[ignore = "item 12: the DFG rung on the device (minutes at ny 62, hours at ny 123)"]
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fn dfg_3d_2z_on_the_device() {
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let ny = env_f("RTX_E3_DFG_NY", 62.0) as usize;
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let h = H / ny as f64;
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let nx = (L / h).round() as usize;
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let nz = ny;
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let t_end = env_f("RTX_E3_DFG_T", 10.0);
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// Explicit stability: CFL 0.3 on U_m and half the viscous limit.
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let dt = (0.3 * h / U_M).min(0.5 * h * h / (6.0 * NU));
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let mut solver = Solver::new(
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Fluid {
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density: RHO,
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viscosity: RHO * NU,
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reference_velocity: U_BAR,
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reference_length: D,
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},
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Parameters {
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corrector_steps: 2,
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tolerance: 1e-8,
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convection_scheme: ConvectionScheme::TvdVanAlbada,
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wall_scheme: WallScheme::CutCell,
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boundaries: Boundaries {
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x1: Side::PressureOutlet,
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..Boundaries::default()
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},
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..Parameters::default()
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},
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);
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solver.set_boundary_velocity(|x, y, z, _t| {
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if x <= 0.0 {
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(inflow(y, z), 0.0, 0.0)
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} else {
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(0.0, 0.0, 0.0)
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}
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});
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solver.set_body(Body::cylinder_z(CX, CY, 0.5 * D));
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let g = Grid::cubic(nx, ny, nz, h);
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let mut field = Field::new(g);
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// Start from the inflow profile everywhere (a faster approach to steady).
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for k in 0..nz {
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for j in 0..ny {
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let u0 = inflow((j as f64 + 0.5) * h, (k as f64 + 0.5) * h);
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for i in 0..=nx {
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field.u[g.uface(k, j, i)] = u0;
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}
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}
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}
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solver.initialize(&mut field);
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let mask_cells = solver.mask().map_or(0, |m| m.fluid_cells());
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println!(
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" DFG 3D-2Z ny {ny}: {nx}×{ny}×{nz} = {} cells ({mask_cells} fluid), h {h:.4e}, dt {dt:.3e}, t_end {t_end}",
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g.cells()
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);
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let mut device = DeviceStep::new(solver, g);
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device.upload(&field);
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let steps = (t_end / dt).ceil() as usize;
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let coef = 2.0 / (RHO * U_BAR * U_BAR * D * H);
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let csv = std::env::var("RTX_E3_DFG_CSV").ok().map(|p| {
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let mut f = std::fs::File::create(p).expect("csv");
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writeln!(f, "t,cd_wall,cl_wall,cd_cv,cl_cv,dp,residual,cg").unwrap();
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f
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});
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let mut csv = csv;
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let sample_every = (steps / 100).max(1);
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let start = std::time::Instant::now();
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let mut last: Option<(f64, f64, f64, f64, f64)> = None;
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let mut settled = false;
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for step in 0..steps {
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let r = device.advance(dt);
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if (step + 1) % sample_every == 0 || step + 1 == steps {
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device.download(&mut field);
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let solver = &device.solver;
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let mask = solver.mask().expect("mask");
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let body = solver.body().expect("body");
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let t = solver.time();
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let fw = mask
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.cut_wall_force(body, &field, RHO * NU, t)
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.expect("wall");
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let margin = 3.0 * D;
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let ci = |x: f64| ((x / h).round() as usize).clamp(2, nx - 2);
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let cj = |y: f64| ((y / h).round() as usize).clamp(2, ny - 2);
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let bx = (
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ci(CX - margin),
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ci(CX + margin),
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cj(CY - 0.15),
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cj(CY + 0.15),
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0,
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nz,
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);
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let fcv = mask.control_volume_force(&field, dt, RHO, RHO * NU, None, bx);
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let zc = 0.5 * H;
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let p_front = mask
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.pressure_at(&field.p, CX - 0.5 * D, CY, zc)
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.unwrap_or(f64::NAN);
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let p_back = mask
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.pressure_at(&field.p, CX + 0.5 * D, CY, zc)
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.unwrap_or(f64::NAN);
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let dp = p_front - p_back;
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let (cd, cl, cd_cv, cl_cv) = (coef * fw[0], coef * fw[1], coef * fcv[0], coef * fcv[1]);
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println!(
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" t {t:8.4}: c_D {cd:.4} (CV {cd_cv:.4}) c_L {cl:.5} (CV {cl_cv:.5}) Δp {dp:.4} residual {:.1e} CG {} [{:.0} s]",
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r.final_residual,
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r.poisson_iterations,
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start.elapsed().as_secs_f64()
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);
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if let Some(f) = csv.as_mut() {
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writeln!(
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f,
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"{t:.5},{cd:.6},{cl:.6},{cd_cv:.6},{cl_cv:.6},{dp:.6},{:.3e},{}",
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r.final_residual, r.poisson_iterations
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)
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.unwrap();
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}
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if let Some((pcd, pcl, _, _, pdp)) = last {
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let rel = ((cd - pcd) / cd)
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.abs()
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.max(((dp - pdp) / dp).abs())
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.max((cl - pcl).abs() / 0.01);
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if rel < 1e-4 && t > 2.0 {
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settled = true;
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}
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}
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last = Some((cd, cl, cd_cv, cl_cv, dp));
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if settled {
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println!(" settled (relative change < 1e-4 between samples)");
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break;
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}
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}
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}
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device.download(&mut field);
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let solver = &device.solver;
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let mask = solver.mask().expect("mask");
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if let Ok(dir) = std::env::var("RTX_E3_DFG_VTK") {
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let path = std::path::Path::new(&dir).join(format!("dfg_2z_ny{ny}.vtk"));
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write_vtk(&path, &field, Some(mask)).expect("vtk");
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println!(" instant written to {}", path.display());
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}
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let (cd, cl, cd_cv, cl_cv, dp) = last.expect("samples");
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println!(
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" FINAL ny {ny}: c_D {cd:.4} (CV {cd_cv:.4}, routes {:.2e} apart) c_L {cl:.5} (CV {cl_cv:.5}) Δp {dp:.4} — reference c_D 6.05–6.25, c_L 0.008–0.010, Δp 0.165–0.175; {:.0} s",
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((cd - cd_cv) / cd).abs(),
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start.elapsed().as_secs_f64()
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);
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if let Some(t) = device.timers() {
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println!(" timers: {t:?}");
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}
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}
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