R8-a: span-uniform coupled FSI2 on embedded3 — DeviceStep snapshot/restore, operator-route load sink, harness fsi2_embedded3.rs

- embedded3 DeviceStep::snapshot/restore (step/device/snapshot.rs): the start-of-step
  device fields + the moving body's host records; a restore rebuilds the R6 persistent
  geometry/classification, the predictor tables, the hierarchy and the guess basis.
  Only called by the new harness (existing paths untouched).
- exchange::set_load_sink: every contribution of the operator load route (p W, wall
  shear, diffusive/convective exchange) with position/component/part; None by default,
  the routes' sums unchanged (slab ny 62 CSV byte-identical to r6_1/base_slab62.csv).
- rtx-fsi feature cuda (= rtx-cfd/cuda) and tests/fsi2_embedded3.rs: the 2D rtx-fea flag
  (35x2 Quad8, TL, Newmark 0.7) drives the capsule's centreline per coupled step; the
  route's contributions are distributed onto the wetted nodes per unit span; Aitken
  subiterations each re-run the fluid step from the snapshot.

Co-Authored-By: Claude Opus 5.5 (1M context) <[email protected]>
This commit is contained in:
Omar Sobh
2026-09-25 18:11:27 -05:00
co-authored by Claude Opus 5.5
parent d63806c0e6
commit 12a27c6fca
7 changed files with 1101 additions and 8 deletions
@@ -0,0 +1,321 @@
//! R8-a: the embedded3 3D cut-cell fluid as the fluid side of a
//! partitioned FSI loop. The body is the embedded flag test's (the circle
//! wall to wall united with a capsule of half-thickness 10 mm around the
//! flag's centreline, its apex on the benchmark's tip A), but the
//! centreline is no longer prescribed: the harness sets it per coupled
//! step from the 2D structure (span-uniform; the centreline's element-corner
//! nodes at reference x 0.25 … 0.59, so the capsule's apex sits on A as the
//! flag test's tip inset puts it), as the pair of lines at the
//! step's start and end; the body's φ and surface velocity at any time in
//! between are the linear blend of the two (the solver asks at the step's
//! two ends only).
//!
//! The loads: the operator route (`Mask::cut_wall_force`) with the R8-a
//! load sink installed — every contribution the route sums, with its
//! position, is returned for the harness to distribute onto the flag.
use std::cell::RefCell;
use std::sync::atomic::{AtomicU64, Ordering};
use std::sync::{Arc, Mutex, RwLock};
use rtx_cfd::solvers::incompressible::ConvectionScheme;
use rtx_cfd::solvers::incompressible::embedded3::exchange::set_load_sink;
use rtx_cfd::solvers::incompressible::embedded3::step::device::{DeviceSnapshot, DeviceStep};
use rtx_cfd::solvers::incompressible::embedded3::{
Body, Boundaries, DeviceSdf, Field, Fluid, Grid, Parameters, Side, Solver, StepResult,
WallScheme,
};
pub const H: f64 = 0.41;
pub const L: f64 = 2.5;
pub const CX: f64 = 0.2;
pub const CY: f64 = 0.2;
pub const R_CYL: f64 = 0.05;
/// The capsule's half-thickness (the flag's half-thickness).
pub const HALF: f64 = 0.01;
pub const RHO: f64 = 1000.0;
pub const NU: f64 = 1e-3;
/// The flag test's CFL velocity (its dt convention, kept for comparability).
const U_CFL: f64 = 2.25;
/// A centreline at time `t`: points (x, y) and their velocities.
#[derive(Clone, Debug)]
pub struct Line {
pub t: f64,
pub pts: Vec<[f64; 2]>,
pub vel: Vec<[f64; 2]>,
}
/// The step's two lines.
pub struct Lines {
pub a: Line,
pub b: Line,
}
impl Lines {
/// The blend at `t` (the start line before `a.t`, the end line after `b.t`).
fn at(&self, t: f64) -> Line {
let eps = 1e-12 * (1.0 + t.abs());
if (t - self.b.t).abs() <= eps || t >= self.b.t || self.b.t <= self.a.t {
return self.b.clone();
}
if t <= self.a.t + eps {
return self.a.clone();
}
let s = (t - self.a.t) / (self.b.t - self.a.t);
let mix = |p: &[[f64; 2]], q: &[[f64; 2]]| -> Vec<[f64; 2]> {
p.iter()
.zip(q)
.map(|(p, q)| [p[0] + s * (q[0] - p[0]), p[1] + s * (q[1] - p[1])])
.collect()
};
assert_eq!(
self.a.pts.len(),
self.b.pts.len(),
"blend needs equal point counts"
);
Line {
t,
pts: mix(&self.a.pts, &self.b.pts),
vel: mix(&self.a.vel, &self.b.vel),
}
}
}
/// Bumped on every `set_lines` (the host closures' per-thread cache key).
static VERSION: AtomicU64 = AtomicU64::new(0);
/// The capsule's signed distance at (x, y) and the centreline velocity at
/// the closest point (the flag test's `flag_2d_recorded`, cached per thread
/// and time).
fn capsule(lines: &RwLock<Lines>, x: f64, y: f64, t: f64) -> (f64, (f64, f64)) {
thread_local! {
static CACHE: RefCell<(u64, u64, Vec<[f64; 4]>)> = const { RefCell::new((u64::MAX, u64::MAX, Vec::new())) };
}
let ver = VERSION.load(Ordering::Acquire);
CACHE.with(|cell| {
let mut c = cell.borrow_mut();
if c.0 != t.to_bits() || c.1 != ver {
let line = lines.read().expect("lines").at(t);
c.2 = line
.pts
.iter()
.zip(&line.vel)
.map(|(p, v)| [p[0], p[1], v[0], v[1]])
.collect();
c.0 = t.to_bits();
c.1 = ver;
}
let pts = &c.2;
let mut best = f64::INFINITY;
let mut v_best = (0.0, 0.0);
for m in 0..pts.len() - 1 {
let [ax, ay, avx, avy] = pts[m];
let [bx, by, bvx, bvy] = pts[m + 1];
let (ex, ey) = (bx - ax, by - ay);
let l2 = ex * ex + ey * ey;
if l2 == 0.0 {
continue;
}
let u = (((x - ax) * ex + (y - ay) * ey) / l2).clamp(0.0, 1.0);
let (px, py) = (ax + u * ex, ay + u * ey);
let d = ((x - px).powi(2) + (y - py).powi(2)).sqrt();
if d < best {
best = d;
v_best = (avx + u * (bvx - avx), avy + u * (bvy - avy));
}
}
(best - HALF, v_best)
})
}
fn cylinder(x: f64, y: f64) -> f64 {
((x - CX).powi(2) + (y - CY).powi(2)).sqrt() - R_CYL
}
/// One load contribution: position, component, part (0 pressure, 1 wall
/// shear, 2 diffusive exchange, 3 convective exchange), force on the body
/// (N, over the whole z extent).
pub type Contribution = ([f64; 3], usize, usize, f64);
pub struct E3Fluid {
pub device: DeviceStep,
pub field: Field,
pub grid: Grid,
pub h: f64,
pub dt: f64,
/// The z extent the loads are divided by (per unit span).
pub width: f64,
pub lines: Arc<RwLock<Lines>>,
sink: Arc<Mutex<Vec<Contribution>>>,
}
impl E3Fluid {
/// The fluid on the benchmark channel at rung `ny`: `nz_slab > 0` the
/// thin slab periodic in z (the flag as a 2D problem), 0 the full 0.41 m
/// duct with slip side walls; the 2D inflow (parabolic in y, Ū 1) in
/// both. `speed` bounds the flag's surface speed (the narrow band).
pub fn build(ny: usize, nz_slab: usize, speed: f64, rest: Line) -> Self {
let h = H / ny as f64;
let nx = (L / h).round() as usize;
let nz = if nz_slab > 0 {
nz_slab
} else {
(H / h).round() as usize
};
// The flag test's step (its CFL velocity; `speed` is the band's bound only).
let dt = (0.3 * h / U_CFL).min(0.5 * h * h / (6.0 * NU))
* super::env_f("RTX_E3FSI_DT_SCALE", 1.0);
let boundaries = if nz_slab > 0 {
Boundaries {
x1: Side::PressureOutlet,
z0: Side::Periodic,
z1: Side::Periodic,
..Boundaries::default()
}
} else {
Boundaries {
x1: Side::PressureOutlet,
z0: Side::SlipWall,
z1: Side::SlipWall,
..Boundaries::default()
}
};
let mut solver = Solver::new(
Fluid {
density: RHO,
viscosity: RHO * NU,
reference_velocity: 1.0,
reference_length: 2.0 * R_CYL,
},
Parameters {
corrector_steps: super::env_f("RTX_E3FSI_CORRECTORS", 3.0) as usize,
inner_stop_factor: super::env_f("RTX_E3FSI_INNER", 1e-3),
tolerance: 1e-8,
convection_scheme: ConvectionScheme::TvdVanAlbada,
wall_scheme: WallScheme::CutCell,
boundaries,
max_surface_speed: Some(speed),
..Parameters::default()
},
);
let inflow = |y: f64| 6.0 * y * (H - y) / (H * H);
solver.set_boundary_velocity(move |x, y, _z, _t| {
if x <= 0.0 {
(inflow(y), 0.0, 0.0)
} else {
(0.0, 0.0, 0.0)
}
});
let lines = Arc::new(RwLock::new(Lines {
a: rest.clone(),
b: rest,
}));
VERSION.fetch_add(1, Ordering::AcqRel);
let (l1, l2, l3) = (lines.clone(), lines.clone(), lines.clone());
let body = Body::from_sdf(move |x, y, _z, t| cylinder(x, y).min(capsule(&l1, x, y, t).0))
.with_surface_velocity(move |x, y, _z, t| {
let (df, (vx, vy)) = capsule(&l2, x, y, t);
if df <= cylinder(x, y) {
(vx, vy, 0.0)
} else {
(0.0, 0.0, 0.0)
}
});
let width = nz as f64 * h;
let body = body.with_device_sdf(move |t| {
let line = l3.read().expect("lines").at(t);
DeviceSdf {
cyl: [CX, CY, R_CYL],
cyl_cut: false,
flag_cut: false,
zc: 0.5 * width,
span: width,
r_edge: h,
half: HALF,
fillet: 0.0,
poly: line.pts,
vel: line.vel,
}
});
solver.set_moving_body(body);
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);
for i in 0..=nx {
field.u[g.uface(k, j, i)] = u0;
}
}
}
solver.initialize(&mut field);
let mut device = DeviceStep::new(solver, g);
device.upload(&field);
println!(
" R8-a fluid: ny {ny}, {nx}×{ny}×{nz} = {} cells ({}), h {h:.4e}, dt {dt:.4e}, speed bound {speed} m/s",
g.cells(),
if nz_slab > 0 {
"slab, periodic z"
} else {
"full duct, slip sides"
}
);
Self {
device,
field,
grid: g,
h,
dt,
width,
lines,
sink: Arc::new(Mutex::new(Vec::new())),
}
}
pub fn time(&self) -> f64 {
self.device.solver.time()
}
/// The step's start and end lines (their times are the lines' own).
pub fn set_lines(&self, a: Line, b: Line) {
*self.lines.write().expect("lines") = Lines { a, b };
VERSION.fetch_add(1, Ordering::AcqRel);
}
pub fn step(&mut self) -> StepResult {
self.device.advance(self.dt)
}
pub fn snapshot(&mut self) -> DeviceSnapshot {
self.device.snapshot()
}
pub fn restore(&mut self, snap: &DeviceSnapshot) {
self.device.restore(snap);
}
/// The operator-route force on the whole body per unit span and the
/// route's contributions (N over the whole z extent).
pub fn loads(&mut self) -> ([f64; 3], Vec<Contribution>) {
self.device.download(&mut self.field);
let t = self.time();
self.sink.lock().expect("sink").clear();
let s = self.sink.clone();
let previous = set_load_sink(Some(Box::new(move |pos, c, part, v| {
s.lock().expect("sink").push((pos, c, part, v));
})));
assert!(previous.is_none(), "a load sink was already installed");
let mask = self.device.solver.mask().expect("mask");
let body = self.device.solver.body().expect("body");
let f = mask
.cut_wall_force(body, &self.field, RHO * NU, t)
.expect("cut wall force");
set_load_sink(None);
let contributions = std::mem::take(&mut *self.sink.lock().expect("sink"));
(
[f[0] / self.width, f[1] / self.width, f[2] / self.width],
contributions,
)
}
}