embedded3 S2-8 instrument: the load routes in PARTS per body — exchange split into diffusive / convective (cut_wall_exchange_parts), a diagnostic x window on every load route (exchange::set_load_window), the flag test as a 2D periodic slab (RTX_E3_FLAG_NZ) with an amplitude knob (RTX_E3_FLAG_AMP, 0 = frozen) and a PARTS summary; cut_wall_force / _per_span moved to exchange.rs (cutwall.rs line cap)
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Co-Authored-By: Claude Fable 5.1 <[email protected]>
This commit is contained in:
co-authored by
Claude Fable 5.1
parent
3f0bd0650a
commit
5e1b3e0731
@@ -65,12 +65,19 @@ fn mode(s: f64) -> f64 {
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/// Centreline deflection and its velocity at arc parameter `s`, time `t`.
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fn deflection(s: f64, t: f64) -> (f64, f64) {
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let w = 2.0 * std::f64::consts::PI * FREQ;
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let amp = amplitude();
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(
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AMP * mode(s) * (w * t).sin(),
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AMP * mode(s) * w * (w * t).cos(),
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amp * mode(s) * (w * t).sin(),
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amp * mode(s) * w * (w * t).cos(),
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)
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}
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/// The tip amplitude: `RTX_E3_FLAG_AMP` (default 0.084; 0 freezes the flag —
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/// the static control of the load routes).
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fn amplitude() -> f64 {
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env_f("RTX_E3_FLAG_AMP", AMP)
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}
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/// Signed distance to the deflected flag's cross-section (a capsule
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/// around the centreline polyline of `n` segments) and the centreline's
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/// transverse velocity at the closest point.
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@@ -131,7 +138,10 @@ fn flag_wake_on_the_device() {
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let periods = env_f("RTX_E3_FLAG_PERIODS", 2.0);
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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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// `RTX_E3_FLAG_NZ=4`: a thin slab periodic in z with the 2D inflow (Ū = 1) — the
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// flag as a 2D problem, minutes per rung: the instrument for the load routes' parts.
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let slab_nz = env_f("RTX_E3_FLAG_NZ", 0.0) as usize;
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let nz = if slab_nz > 0 { slab_nz } else { ny };
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let r_edge = h;
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let dt_cfl = 0.3 * h / (U_M.max(2.0 * std::f64::consts::PI * FREQ * AMP));
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// `RTX_E3_FLAG_DT_SCALE` scales the step (the dt ladder of the loads).
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@@ -155,18 +165,36 @@ fn flag_wake_on_the_device() {
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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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boundaries: if slab_nz > 0 {
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Boundaries {
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x1: Side::PressureOutlet,
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z0: Side::Periodic,
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z1: Side::Periodic,
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..Boundaries::default()
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}
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} else {
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Boundaries {
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x1: Side::PressureOutlet,
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..Boundaries::default()
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}
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},
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// The narrow band: the flag's tip speed bounds the surface motion.
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max_surface_speed: Some(2.0 * std::f64::consts::PI * FREQ * AMP * 1.05),
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max_surface_speed: Some(
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(2.0 * std::f64::consts::PI * FREQ * amplitude() * 1.05).max(1e-3),
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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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let inflow_at = move |y: f64, z: f64| {
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if slab_nz > 0 {
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6.0 * y * (H - y) / (H * H)
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} else {
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inflow(y, z)
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}
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};
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solver.set_boundary_velocity(move |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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(inflow_at(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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@@ -186,7 +214,7 @@ fn flag_wake_on_the_device() {
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let mut field = Field::new(g);
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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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let u0 = inflow_at((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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@@ -217,9 +245,17 @@ fn flag_wake_on_the_device() {
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let last_period_start = t_end - period;
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let mut next_phase = 0;
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let mid = nz / 2;
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let slab = (mid - 2, mid + 2);
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let slab = if slab_nz > 0 {
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(0, nz)
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} else {
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(mid - 2, mid + 2)
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};
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let width = nz as f64 * h;
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let start = std::time::Instant::now();
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let mut drag_rec_sum = 0.0;
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// The routes' PARTS over the whole body (x, per unit width): operator
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// pressure / shear / exchange, reconstructed pressure / shear.
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let mut parts = [[0.0_f64; 6]; 3];
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let (mut drag_sum, mut lift_min, mut lift_max, mut samples) =
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(0.0, f64::INFINITY, f64::NEG_INFINITY, 0usize);
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let mut worst_residual = 0.0_f64;
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@@ -283,6 +319,30 @@ fn flag_wake_on_the_device() {
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.unwrap();
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}
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if t >= last_period_start {
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use rtx_cfd::solvers::incompressible::embedded3::exchange::set_load_window;
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// whole body, the cylinder (x < 0.252), the flag
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for (w, window) in [None, Some((0.0, 0.252)), Some((0.252, 10.0))]
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.into_iter()
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.enumerate()
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{
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set_load_window(window);
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let (po, so) = mask
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.cut_wall_force_parts(body, &field, RHO * NU, t)
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.expect("parts");
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let (xd, xc) = mask
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.cut_wall_exchange_parts(body, &field, RHO * NU, RHO, t, None)
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.expect("exchange");
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let (pr, sr) = mask
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.cut_wall_force_reconstructed_parts(body, &field, RHO * NU, t, None)
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.expect("reconstructed parts");
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for (acc, v) in parts[w]
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.iter_mut()
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.zip([po[0], so[0], xd[0], xc[0], pr[0], sr[0]])
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{
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*acc += v / width;
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}
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}
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set_load_window(None);
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drag_sum += fs[0];
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drag_rec_sum += fr[0];
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lift_min = lift_min.min(fs[1]);
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@@ -306,6 +366,21 @@ fn flag_wake_on_the_device() {
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next_phase,
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start.elapsed().as_secs_f64()
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);
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let n = samples.max(1) as f64;
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for (name, q) in ["whole body", "cylinder", "flag"].iter().zip(parts) {
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println!(
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" PARTS ny {ny} amp {:.3} {name} (x, N/m of width): operator pressure {:.2} + shear {:.2} + exchange diffusive {:.2} + convective {:.2} = {:.2}; reconstructed pressure {:.2} + shear {:.2} = {:.2}",
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amplitude(),
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q[0] / n,
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q[1] / n,
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q[2] / n,
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q[3] / n,
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(q[0] + q[1] + q[2] + q[3]) / n,
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q[4] / n,
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q[5] / n,
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(q[4] + q[5]) / n
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);
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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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