rustytorch/crates/specialized/rtx-cfd/tests/embedded3_dfg_2d1_host.rs

//! S2-5 host ladder: DFG 2D-1 (Re 20) on a periodic-z slab of 4 cells with
//! every knob of the cut wall read from the environment — the instrument
//! for host-only prototypes (`RTX_E3_PRESSURE_CENTROID=1`). Reference
//! c_D 5.57954, c_L 0.010619, Δp 0.117520. `RTX_E3_DFG_NY` (default 62).
use rtx_cfd::solvers::incompressible::ConvectionScheme;
use rtx_cfd::solvers::incompressible::embedded3::{
    Body, Boundaries, Field, Fluid, Grid, Parameters, Side, Solver, WallScheme,
};

const H: f64 = 0.41;
const L: f64 = 2.2;
const D: f64 = 0.1;
const CX: f64 = 0.2;
const CY: f64 = 0.2;
const U_M: f64 = 0.3;
const U_BAR: f64 = 2.0 / 3.0 * U_M;
const RHO: f64 = 1.0;
const NU: f64 = 1e-3;

fn inflow(y: f64, _z: f64) -> f64 {
    4.0 * U_M * y * (H - y) / (H * H)
}

#[test]
#[ignore = "host DFG at ny 31 with the routes split (about half an hour)"]
fn dfg_2d1_on_the_host() {
    let ny: usize = std::env::var("RTX_E3_DFG_NY")
        .ok()
        .and_then(|v| v.parse().ok())
        .unwrap_or(62);
    let h = H / ny as f64;
    let nx = (L / h).round() as usize;
    let nz = 4;
    let lz = nz as f64 * h;
    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,
                z0: Side::Periodic,
                z1: Side::Periodic,
                ..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)
        }
    });
    solver.set_body(Body::extruded(
        rtx_cfd::solvers::incompressible::EmbeddedBody::circle(CX, CY, 0.5 * D),
        lz,
    ));
    let g = Grid::cubic(nx, ny, nz, h);
    let mut field = Field::new(g);
    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 coef = 2.0 / (RHO * U_BAR * U_BAR * D * lz);
    let steps = (12.0 / dt).ceil() as usize;
    let start = std::time::Instant::now();
    let mut last = (0.0, 0.0);
    for step in 0..steps {
        let r = solver.advance(&mut field, dt);
        if (step + 1) % (steps / 20).max(1) == 0 || step + 1 == steps {
            let t = solver.time();
            let mask = solver.mask().unwrap();
            let body = solver.body().unwrap();
            let mu = RHO * NU;
            let (po, so) = mask.cut_wall_force_parts(body, &field, mu, t).unwrap();
            let ex = mask
                .cut_wall_exchange_force(body, &field, mu, RHO, t, None)
                .unwrap();
            let (pr, sr) = mask
                .cut_wall_force_reconstructed_parts(body, &field, mu, t, None)
                .unwrap();
            let margin = 1.5 * 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, mu, None, bx, false);
            let cd = |f: [f64; 3]| coef * f[0];
            println!(
                "  t {t:7.3}: c_D operator {:.4} (p {:.4} + s {:.4} + exchange {:.4}) | reconstructed {:.4} (p {:.4} + s {:.4}) | box {:.4} c_L {:.5} Δp {:.5}; residual {:.1e} [{:.0} s]",
                cd(po) + cd(so) + cd(ex),
                cd(po),
                cd(so),
                cd(ex),
                cd(pr) + cd(sr),
                cd(pr),
                cd(sr),
                cd(fcv),
                coef * (po[1] + so[1] + ex[1]),
                mask.pressure_at(&field.p, CX - 0.5 * D, CY, 0.5 * lz)
                    .unwrap_or(f64::NAN)
                    - mask
                        .pressure_at(&field.p, CX + 0.5 * D, CY, 0.5 * lz)
                        .unwrap_or(f64::NAN),
                r.final_residual,
                start.elapsed().as_secs_f64()
            );
            let now = (cd(po) + cd(so) + cd(ex), cd(fcv));
            if (now.0 - last.0).abs() < 1e-4 * now.0.abs()
                && (now.1 - last.1).abs() < 1e-4 * now.1.abs()
                && t > 2.0
            {
                println!("  settled");
                break;
            }
            last = now;
        }
    }
}