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4aec4e589d |
rtx-cfd/rtx-fsi: the FlowField->clawview exporter — real FSI fields through the viewer, end to end
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The march gains RTX_FSI{2,3}_FFLD (MarchConfig::ffld_dir, off by
default): every snap_every committed steps (10 when SNAPEVERY is 0),
dump the committed FlowField (FlowField::save, bit-exact), the solver's
own fluid-cell mask and the interface polygon as text sidecars, plus an
index.csv. Reporting-only after acceptance; the FSI2 default with the
knob off reproduces every printed digit of the warm-start baseline
(uy 3.4921 +- 3.5109, conservation 8.25e-12).
The exporter (rtx-cfd examples/ffld_to_vtk): a dump directory ->
clawview-readable legacy VTK — per-snapshot 2D triangle meshes (one
selectable point scalar --field p|umag|vort, the 0/1 fluid mask as
integer CELL_DATA) and an optional space-time volume (--spacetime:
frames stacked along z = time, prisms split to tets, POINT_DATA phi),
which clawview's slice-plane animation plays as a transient movie.
Verified end to end with REAL fields, not synthetic: a 29-frame FSI3
release-transient dump (t 4.0 -> 4.1, 64 MB) exported to 29 snapshots
+ a 984,312-tet space-time volume; the clawview server loaded both
(176,320 nodes volume; 23,877-node snapshots) and served live
cross-sections (time slices), vorticity isosurfaces and contours from
them. The check caught two real viewer-contract constraints now
encoded in the exporter: clawview's legacy-VTK path parses CELL_DATA
scalars as INTEGER markers only, and supports exactly ONE point scalar
(all POINT_DATA blocks append into `phi`) — multi-field snapshots need
the .clwv route, out of scope here.
Closes the top open thread of the fifteenth-session handoff (the
FSNP/FlowField->viewer exporter); the mesh-repo push and the claw-gds
cargo feature remain clawview-side items.
Co-Authored-By: Claude Fable 5 <[email protected]>
Claude-Session: https://claude.ai/code/session_01X2GmJXeQ2njUecEKiJZ1G2
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327da7ff47 |
rtx-cfd: multigrid-PCG projection — 30x faster, same answers — and the CFD1 refinement study
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Falsifier 4 of the Turek–Hron geometry decision fired (the SOR projection
cost 0.09 s/step at 250x41 and an hour per run at 5 mm); this answers it.
solvers::incompressible::poisson: PoissonProblem (cell-centred five-point
SPD operator as per-cell face coefficients + Dirichlet diagonal extra +
active mask) and solve_multigrid_pcg — conjugate gradient preconditioned
by one V-cycle of geometric multigrid: aggregation by 2 per direction (odd
sizes absorbed, coarse cell active iff any child is), the Galerkin coarse
operator for piecewise-constant prolongation / summation restriction,
symmetric Gauss–Seidel smoothing, coarse correction scaled by 2 (Braess's
under-correction of unsmoothed aggregation; scalar, so the preconditioner
stays symmetric and positive on range(A)), L1 TRUE-residual stop with a
stagnation guard. Singular systems are handled per connected component of
the active cells (mean projection and level per pure-Neumann component;
the anchor's component to p[anchor] = 0). PoissonSolverKind::{Sor,
Multigrid} on PisoParameters / EmbeddedParameters; Sor is the default and
its code is byte-for-byte untouched; an unconverged multigrid solve falls
back to the SOR sweeps for that projection.
Verified (poisson/tests.rs, tests/poisson_equivalence.rs):
- PCG iterations to cut the residual 1e-8 on the closed Neumann box at
32^2..256^2: 4, 4, 4, 4; ragged masked domains 8/8/8;
- manufactured recoveries to ~1e-14; Galerkin identity A_c v = R A P v to
7e-15 on every level (masked, outlet column, non-uniform conductances);
V-cycle symmetric to 1e-14; NaN-poisoned inactive cells untouched;
- two Neumann components with opposite imbalances, and a Dirichlet
component beside an imbalanced Neumann one (review scenarios): converge,
each component right up to its own constant;
- speed vs plain SOR at the same stop: 22.7x (128^2), 41x (256^2);
- same answers as SOR: PISO MMS 4.6e-8 relative, Taylor–Green divergence
1.4e-9 every step, embedded-circle MMS 7e-8, no-body bit-identity with MG
on both solvers, channel+outlet+circle 1.4e-10; CFD1 loads identical to
four digits at 0.003 s/step vs 0.094 (30x).
CFD1 refinement study (tests/turek_hron_cfd.rs, three grids, 257 s):
h = 10 / 6.6 / 5 mm -> control-volume drag 15.6156 / 15.2829 / 15.0988 vs
14.2929 (+9.25 / +6.93 / +5.64%), apparent order 0.71, Richardson
extrapolate 14.04; surface route and lift not monotone (flag 2/3/4 cells
thick) — the test asserts the measured band at the finest grid.
Built with a 4-agent workflow (core, integration, refinement study,
adversarial review); the review found no defects and four risks, three
fixed here (per-component projection, one symmetric smoother-sweep
parameter, acting on `converged` with an SOR fallback) and one recorded
(isotropic aggregation loses grid-independence on anisotropic cells).
rtx-cfd 301 -> 318 green.
Co-Authored-By: Claude Fable 5 <[email protected]>
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4d88dc0584 | Initial commit |