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Author SHA1 Message Date
ClaudeandClaude Opus 5.5 1fa498c7d7 kernels: shared block-window to global coordinate helper
BlockStep (slot-reservoir wall rows) and BlockChannelStep computed the
global cell of a block-window cell with the same four lines.
block_global_xy (core/layout.cuh, 2D, __forceinline__) now holds them;
both kernels call it with their own domain width. Same integer
operations: no numerical, ABI or scheduling change. The slot-reservoir
kernel layout is unchanged (no split).

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
2026-10-21 01:24:27 +00:00
ClaudeandClaude Opus 5.5 781333407e kernels: one shared unforced MRT collision for blocked, channel and patch paths
BlockStep, BlockChannelStep and refinement.cu patch_collide each carried
the same compute_rho_u -> omega clamp -> collide_mrt_no_force sequence.
collide_mrt_unforced (collision_mrt.cuh, __forceinline__) now holds it
once; the three sites call it. Same operations in the same order: no
numerical, ABI or SRT change. The host source contract now requires one
helper definition and exactly one call per file, and forbids the old
inline sequence.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
2026-10-21 01:15:47 +00:00
ClaudeandCodex 750e8a483e test: DFG Re20 steady rule as agreed (10 % range, 2 % slope, window-mean verdict)
Supersedes 71221837. Samples every t* 0.5 (interval-mean forces), trailing
t* 50..60 window (21 samples); range <= 10 % and |slope*window| <= 2 % of
each official band width. Verdict on the window mean with the distance to
the nearest band edge. Our engineering rule, frozen before any run.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
(cherry picked from commit 869d60d78e)
2026-10-20 21:59:15 +08:00
ClaudeandCodex 6a03f463bc test: DFG Re20 steady rule per review (1 % band, range and slope, 0.5 s samples)
Samples every 0.5 s at synchronized root steps; trailing 5 s window (11
samples); range and |slope*window| each at most 1 % of the official band
width. States the fluid-on-cylinder force sign, reports cd_positive,
defaults to the refined case and uses the review's label.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
(cherry picked from commit 71221837f9)
2026-10-20 21:59:15 +08:00
ClaudeandCodex 46dc6ba086 test: add DFG 2D-1 Re20 runner against official reference intervals
Reuses the pinned Re100 runner and helpers unchanged; sets only the
lattice viscosity for Re 20. Reports Cd, Cl and p_diff (dp * 0.04 for
U = 0.2 m/s), a steady rule frozen before any run (window ranges at most
a tenth of each official interval width) and no interval verdict when
not steady. Declares the pressure-NEQ outlet and Zou-He inlet deviations.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
(cherry picked from commit 9b8ff90609)
2026-10-20 21:59:15 +08:00
ClaudeandCodex e1efc18274 test: follow the recursive _advance in three-level feed checks
baba5e0 replaced _advance_child with _advance(index, parent_buffer) driven
from _hop; the two feed-order tests still patched the removed method.
Patch _advance and record only index 2 (L1 hop feeding L2); assertions,
expected order and the stale-feed negative control are unchanged.

Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
(cherry picked from commit 3f47436073)
2026-10-20 21:57:57 +08:00
ClaudeandClaude Opus 5.5 9660894a1b docs: checkpoint save/load scope and read_surface_exchange wording
Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
2026-10-20 13:38:30 +00:00
ClaudeandClaude Opus 5.5 ba3772e3b8 docs: record cut-link ownership and read_surface_exchange changes from 87c3a31
Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com>
2026-10-20 13:29:44 +00:00
CodexandFrank14f b4692e6ec4 test: select single-case resolution and compact refinement 2026-10-19 23:55:26 +08:00
CodexandFrank14f 5731c5171b test: add optional public macro CV observations 2026-10-19 22:43:22 +08:00
CodexandFrank14f 05de02ee60 test: parameterize matched public MRT Jet diagnostics 2026-10-19 22:43:22 +08:00
CodexandFrank14f 87c3a3165e fix: validate passive boundary ownership and expose Jet exchange 2026-10-19 22:43:22 +08:00
22 changed files with 1167 additions and 105 deletions
+35
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@@ -0,0 +1,35 @@
# Compatibility and API changes
Changes that can make a previously accepted setup or call behave differently.
Each entry names the commit, the affected entry points and the observable result.
## 87c3a31: cut-link ownership is validated for every body
`validate_cut_link_ownership` (`body/preprocess/flag_overlay.py`) now runs for
passive bodies as well as Jet/aperture bodies. Every cut link must have an
active fluid receiver (FLUID set, SOLID clear), and each `(receiver, direction)`
population may have only one writer.
Rejected with `ValueError`, before flags, populations or device buffers change:
1. Overlapping or touching passive solids whose cut links write the same
population ("Boundary requires unique cut-link writers").
2. A body whose cut-link receiver is a non-fluid cell, e.g. a channel wall row
or the inlet/outlet column ("Cut links must have active fluid receivers").
Both were previously accepted silently for passive bodies; the interpolated
boundary then had undefined results. The rules apply to the cut links of all
bodies together, so a passive body overlapping a Jet body is rejected as well.
The check runs in `Simulation.initialize`, runtime body sync (`sync_bodies`),
checkpoint save and checkpoint load (`common/checkpoint.py`). Load validates
before restoring anything, so a checkpoint whose saved geometry violates either
rule no longer restores; rebuild the geometry with separated bodies.
## 87c3a31: `Simulation.read_surface_exchange` accepts Jet-driven bodies
`read_surface_exchange(id)` previously required `SurfaceActuation` on the body.
It now also accepts bodies that own Jet aperture links, including Jets with zero
or negative amplitude (the aperture test is geometric). Bodies with neither
`SurfaceActuation` nor aperture links still raise
`ValueError("Body has no surface actuation")`. The value is unchanged: the latest
step's wall/aperture exchange, not total nozzle force.
+49
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@@ -0,0 +1,49 @@
# DFG 2D-1 (Re 20) against the official reference intervals
`tests/validation/run_dfg_re20.py` runs the steady DFG 2D-1 case on the refined
channel root (D40 root, D80 wide fine patch) and on the uniform D80 grid. Geometry,
inflow, initial state, layout and observation are those of the pinned Re100 runner
(`run_refined_dfg.py`, `re100_helpers.py`, both unchanged); only the lattice
viscosity is set for Re 20 (root tau 0.56, fine 0.62, uniform 0.62, lattice speed 0.01).
Label: "compared against the official reference bands", not a full benchmark
certification: the outlet is pressure-NEQ (`neq_extrap`), not do-nothing, and the
inlet is local Zou-He.
## Quantities
- Cd = 2 Fx / (rho U^2 D), Cl = 2 Fy / (rho U^2 D), interval means over each sample.
- p_diff = p(0.15, 0.2) - p(0.25, 0.2), linear extrapolation to the exact surface
points (`re100_helpers.pressure_probes`). The helper returns dp / (rho U^2) in
scaled units; p_diff = dp * 0.04 for U = 0.2 m/s, rho = 1. Both are reported.
- Official intervals (Schaefer & Turek 1996): Cd [5.57, 5.59], Cl [0.0104, 0.0110],
p_diff [0.1172, 0.1176].
## Bounds and steady rule (frozen before any run)
- End time t* = 60 (30 s physical): 240,000 refined root steps, 480,000 uniform steps.
- One sample every t* = 0.5 (0.25 s) at the end of a synchronized root step; Cd and
Cl are interval means. Trailing window t* 50..60 inclusive (21 samples).
- Steady rule (our engineering choice, not official): in the window, for each of Cd,
Cl, p_diff, max - min <= 10 % and |least-squares slope x window| <= 2 % of its
official interval width (range 2e-3 / 6e-5 / 4e-5; slope 4e-4 / 1.2e-5 / 8e-6).
Absolute limits, so the small Cl is never a divisor. Never relaxed after a run.
- The verdict uses the window mean; the distance to the nearest interval edge is
reported for each quantity (negative outside).
- Force sign: fluid on cylinder, x along the inflow, y up from the bottom wall; Cd > 0
and the official Cl > 0 (`cd_positive` is reported).
- Not steady at t* = 60: status `NOT_STEADY`, no interval verdict. Health limits
(Mach <= 0.2, rho in [0.5, 1.5]) stop the run with `UNHEALTHY`.
- Steady: `WITHIN_INTERVALS` or `OUTSIDE_INTERVALS`, with the per-quantity verdict.
## Run
```
python tests/validation/run_dfg_re20.py --output <new-dir> --plan
CUDA_VISIBLE_DEVICES=<n> python tests/validation/run_dfg_re20.py --case both \
--collision SRT --output <new-dir> --max-wall-seconds <cap>
```
The uniform D80 control separates method error from refinement error. `--plan` writes `plan.json` only. A GPU run writes `plan.json` and `result.json`
(per case: lattice parameters, every sample, window ranges, status, verdict).
Host contract tests: `tests/unit/test_dfg_re20.py`.
+59
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@@ -56,3 +56,62 @@ Root must independently review and admit any execution. An admitted paired pilot
the existing watchdog, device selection, `--gpu-gates-approved`, positive
`--max-wall-seconds` and a new output directory, adding only `--exchange-window` to the
selected collision's pilot command. No GPU or remote action was performed for this patch.
## Public Jet diagnostic option
`--collision MRT --exchange-window --jet-scenario zero|fixed|reverse` selects
unshifted FP32, no LES, constant transfer on both existing public backends. Default
`none` and the historical manifests remain unchanged. `zero` registers both Jets at
zero amplitude and retains every existing DFG verdict, including pressure. `fixed`
uses outward radial parabolic sectors at pi/2 and 3pi/2, half-width pi/12, peaks
(+.001,-.001). Both use the existing D40/D80 geometry and U=.01. Sector origins are
(80.5,81) in root edge coordinates and (160,160.5) in uniform node coordinates;
radial extent is [0,1.005R]. `reverse` keeps those peaks through t*=300, updates both
public setters at that completed boundary, and continues to 305 with opposite signs.
Fixed diagnostic windows are 250–260, 260–270, 270–280, 280–290 and 290–300; reversal
adds 300–305. Histories retain exact interval endpoints and root/uniform lattice
impulses. The refined window uses total exchange; uniform uses public `read_force`
batch averages. Driven windows report mean/min/max/RMS Cd/Cl without applying DFG
reference or periodicity gates. Exit zero means healthy execution, not qualification;
`matched_case_pass` remains false. No independent CV or stress-load claim is made.
This opt-in records current source/helper hashes with the existing manifest format,
checkout revision/dirty state and runner hash. Pilot/full must match that snapshot
and the exact scenario. It does not relabel current source as historical evidence.
Use the existing bounded plan/pilot/full commands with the three option flags above;
full requires the matching completed t*=5 paired pilot. `step_seconds` includes force
readback; observation/overhead and total wall time are separate, not kernel throughput.
Add `--observe-cv` to record independent scalar control-volume samples from the
already downloaded public macros. The pilot exercises this path at t*=.02..5;
full records 501 endpoints at 290..300. Each `cv_history.jsonl` row contains actual
root time, preceding interval start/duration/impulse, and two inventories/outward
fluxes ordered [mass,Px,Py]. Exclude the first row's preceding impulse: that row
supplies the initial inventory. Uniform native impulse converts by .5² to root
units; refined ledger impulse is already in root units. Explicit native-aligned
contours differ by .25 root cells in x and are recorded in the plan. Cropping
retains the two-cell face-gradient stencils. No fields or per-link arrays are saved.
`cv_observation_seconds` is the CV portion of observation/overhead time. Helper hash
and the observation flag must match pilot/full. Time integration, temporal
coarsening and any physical assessment remain separate offline work.
## Bounded resolution and placement controls
Defaults remain `--case both --uniform-diameter 80 --placement wide`. Single-case
runs use `--case uniform` or `--case refined` and never report a matched-case pass.
Their own reference/periodicity or driven-diagnostic results remain available.
A single zero-Jet full run exits successfully only when its periodicity and the
unchanged complete DFG reference verdict pass; driven completion is not qualification.
The D160 option requires `--case uniform --uniform-diameter 160` and an explicit
public Jet scenario. U and Jet speeds stay .01 and ±.001; viscosity is .016,
grid 3521×658, center (320,320.5), radius80. CV uses root spacing/time factor .25,
origin (.375,.75), impulse factor .0625, root viscosity .004, and x-face shift .125.
`--case refined --placement compact` selects root bounds (48,48,128,128), fine
168×168 and origin (46,46), with the same D40/fineD80 body/Jet resolution. Its CV
contours are (52,52,112,112) and (50,50,120,120); complete face-gradient stencils
are clear of both solids and the transfer footprint. Compact is refined-only.
CV metadata gives each grid's spacing/origin/contours explicitly. Case, uniform
diameter and placement must match the newly completed pilot in every receipt.
+2 -5
View File
@@ -216,11 +216,8 @@ def surface_link_velocity(objects, cfg, flags, fluid_idx, dir, body_id, rx, ry,
enabled = [obj for obj in objects if obj.surface_actuation is not None]
if not enabled and not jets:
return None, None
from ..lbm.descriptors import FLUID, SOLID
if np.any((flags[fluid_idx] & FLUID) == 0) or np.any(flags[fluid_idx] & SOLID):
raise ValueError("Surface cut links must have active fluid receivers")
if len(np.unique(fluid_idx.astype(np.uint64)*cfg.nq+dir)) != len(dir):
raise ValueError("Surface boundary requires unique cut-link writers")
from .preprocess.flag_overlay import validate_cut_link_ownership
validate_cut_link_ownership(flags, fluid_idx, dir, cfg.nq)
surface_velocity = np.zeros((len(dir), 2), np.float32)
surface_aperture = np.zeros(len(dir), bool)
for obj in enabled:
+17 -12
View File
@@ -27,7 +27,7 @@ import pycuda.driver as cuda
from .objects import SimObject
from .registry import BodyRegistry
from .preprocess.flag_overlay import merge_flag_masks
from .preprocess.flag_overlay import merge_flag_masks, validate_cut_link_ownership
from ..cuda.compiler_v2 import obs_layout
from ..cuda.obs_layout import ObsLayout
from ..lbm.descriptors import (
@@ -369,9 +369,9 @@ class ObjectManager:
Args:
objects: List of SimObject instances to process.
domain_flags: Optional uint16 flags for donor-cell classification.
domain_flags: Optional uint16 flags for receiver/donor classification.
sensor_cell_counts_out: Int array to fill with per-object sensor
cell counts. If provided, ``fill(0)`` is called first.
cell counts after the full geometry has passed validation.
hits_out: List that receives one FP64 (n, 2) array of true hit
points row-aligned with the cut-link columns (for Jets).
@@ -394,8 +394,8 @@ class ObjectManager:
active_fluid = ((domain_flags & FLUID) != 0) & ((domain_flags & SOLID) == 0)
force_owners: set[int] = set()
if sensor_cell_counts_out is not None:
sensor_cell_counts_out.fill(0)
sensor_counts = (np.zeros_like(sensor_cell_counts_out)
if sensor_cell_counts_out is not None else None)
ez = None
if self.cfg and self.cfg.is_d3q19:
@@ -430,9 +430,9 @@ class ObjectManager:
if len(cells) > 0:
s_cells.append(cells)
s_ids.append(ids)
if (sensor_cell_counts_out is not None
and 0 <= obj.obj_id < sensor_cell_counts_out.size):
sensor_cell_counts_out[obj.obj_id] = int(len(cells))
if (sensor_counts is not None
and 0 <= obj.obj_id < sensor_counts.size):
sensor_counts[obj.obj_id] = int(len(cells))
if obj.is_force_region and hasattr(obj, 'get_sensor_list'):
cells, ids = obj.get_sensor_list(self.nx, self.ny, self.nz)
keep = active_fluid[cells]
@@ -461,8 +461,9 @@ class ObjectManager:
r_fr_ids = np.concatenate(fr_ids) if fr_ids else np.zeros(0, dtype=np.int32)
r_hit = np.concatenate(cl_hit) if cl_hit else np.zeros((0, 2))
if hits_out is not None:
hits_out.append(r_hit)
# Passive walls need the same ownership guarantees as driven walls.
# Overlapping solids are not a supported union-boundary operation.
validate_cut_link_ownership(domain_flags, r_idx, r_dir, self.nq)
if self.jets or any(obj.surface_actuation is not None for obj in objects):
# Reject unresolved apertures/ownership before sync or restart mutates state.
from ..lbm.curved_links import CurvedLinkSoA
@@ -470,6 +471,11 @@ class ObjectManager:
links.assign_host(r_idx, r_dir, r_q, r_bid, r_rx, r_ry, r_rz, r_fallback)
links.assign_surface(objects, self.cfg, domain_flags, jets=self.jets, hits=r_hit)
if sensor_cell_counts_out is not None:
sensor_cell_counts_out[:] = sensor_counts
if hits_out is not None:
hits_out.append(r_hit)
return (
r_idx, r_dir, r_q, r_bid,
r_rx, r_ry, r_rz, r_fallback,
@@ -487,8 +493,6 @@ class ObjectManager:
the caller has already prepared and uploaded the final flag field
for this geometry, such as during initialization.
"""
self._telemetry_field = field
next_flags = self.build_flags(field.build_channel_flags()) if rebuild_flags else field.flag
hits = []
@@ -499,6 +503,7 @@ class ObjectManager:
fr_cells, fr_obj_id,
) = self.build_compact_lists(domain_flags=next_flags, hits_out=hits)
self._telemetry_field = field
if rebuild_flags:
field.flag = next_flags
field.upload_flags()
+10 -1
View File
@@ -1,6 +1,6 @@
# CelerisLab/body/preprocess/flag_overlay.py
"""
Flag overlay: merge per-object flag masks onto a clean domain base.
Flag overlay and cut-link ownership checks against the merged domain.
"""
from __future__ import annotations
@@ -12,6 +12,15 @@ import numpy as np
from ...lbm.descriptors import FLUID, SOLID, SENSOR_FLAG, FRC_REGION
def validate_cut_link_ownership(flags, fluid_idx, directions, nq):
"""Reject solid receivers and multiple writers to one population."""
if np.any((flags[fluid_idx] & FLUID) == 0) or np.any(flags[fluid_idx] & SOLID):
raise ValueError("Cut links must have active fluid receivers")
writers = fluid_idx.astype(np.uint64) * nq + directions
if len(np.unique(writers)) != len(directions):
raise ValueError("Boundary requires unique cut-link writers")
def merge_flag_masks(
base: np.ndarray,
masks: List[np.ndarray],
+3 -9
View File
@@ -168,21 +168,15 @@ extern "C" __global__ void BlockStep(const fpxx* in, fpxx* out, unsigned int hal
stream_pull_load(k, f, in + base, j);
if (cell_kind == KIND_ACTIVE) {
if (d_block_wall.nx != 0) {
const unsigned int bx = NX - 2 * halo, by = NY - 2 * halo;
const unsigned int nbx = d_block_wall.nx / bx;
const unsigned int gx = (blockIdx.z % nbx) * bx + x - halo;
const unsigned int gy = (blockIdx.z / nbx) * by + y - halo;
unsigned int gx, gy;
block_global_xy(x, y, halo, d_block_wall.nx, gx, gy);
if (gy == 1)
reconstruct_bottom_velocity(f, 0.0f, bottom_wall_normal_velocity(
gx, d_block_wall.nx, d_block_wall.slot_width, d_block_wall.amplitude));
else if (gy == d_block_wall.ny - 2) reconstruct_top_reservoir(f, RHO);
}
#if COLLISION_MODEL == 2
// Uniform MRT sequence (collide_dispatch, zero forcing); SRT path below unchanged.
float rho, ux, uy;
compute_rho_u(f, rho, ux, uy);
collide_mrt_no_force(f, rho, ux, uy,
fminf(OMEGA_COLLISION_MAX, fmaxf(OMEGA_COLLISION_MIN, d_params.omega)));
collide_mrt_unforced(f); // SRT path below unchanged.
#else
float rho, ux, uy, feq[NQ];
compute_rho_u(f, rho, ux, uy);
@@ -53,6 +53,18 @@ __device__ __forceinline__ void index_from_thread(unsigned int& x,
k = (unsigned long)y * NX + x;
}
// Global cell of window cell (x, y) in block blockIdx.z of a row-major,
// full-domain block layout domain_nx cells wide. NX/NY are the local strides.
__device__ __forceinline__ void block_global_xy(unsigned int x, unsigned int y,
unsigned int halo, unsigned int domain_nx,
unsigned int& gx, unsigned int& gy)
{
const unsigned int bx = NX - 2 * halo, by = NY - 2 * halo;
const unsigned int nbx = domain_nx / bx;
gx = (blockIdx.z % nbx) * bx + x - halo;
gy = (blockIdx.z / nbx) * by + y - halo;
}
// ---------------------------------------------------------------------------
// Neighbor list (periodic BCs via modular arithmetic)
// ---------------------------------------------------------------------------
@@ -114,6 +114,16 @@ __device__ __forceinline__ void collide_mrt_no_force(float* __restrict__ g,
collide_mrt(g, rho, ux, uy, Fin, omega);
}
// Unforced MRT with the clamped device omega, as in collide_dispatch with zero
// forcing. Shared by the blocked, channel-root and dense-patch collisions.
__device__ __forceinline__ void collide_mrt_unforced(float* __restrict__ g)
{
float rho, ux, uy;
compute_rho_u(g, rho, ux, uy);
collide_mrt_no_force(g, rho, ux, uy,
fminf(OMEGA_COLLISION_MAX, fmaxf(OMEGA_COLLISION_MIN, d_params.omega)));
}
#elif LATTICE_MODEL == LATTICE_D3Q19
__device__ __forceinline__ void collide_mrt(float* __restrict__ g,
+1 -4
View File
@@ -37,10 +37,7 @@ __device__ unsigned int incoming_counts[NQ * TOTAL_CELLS];
__device__ __forceinline__ void patch_collide(float* f, unsigned long k) {
#if COLLISION_MODEL == 2
float rho, ux, uy;
compute_rho_u(f, rho, ux, uy);
collide_mrt_no_force(f, rho, ux, uy,
fminf(OMEGA_COLLISION_MAX, fmaxf(OMEGA_COLLISION_MIN, d_params.omega)));
collide_mrt_unforced(f);
#else
float rho, ux, uy, feq[NQ];
compute_rho_u(f, rho, ux, uy);
@@ -15,10 +15,8 @@ extern "C" __global__ void BlockChannelStep(
unsigned int x, y; unsigned long k;
index_from_thread(x, y, k);
if (x < halo || y < halo || x >= NX - halo || y >= NY - halo) return;
const unsigned int bx = NX - 2 * halo, by = NY - 2 * halo;
const unsigned int nbx = d_block_channel.nx / bx;
const unsigned int gx = (blockIdx.z % nbx) * bx + x - halo;
const unsigned int gy = (blockIdx.z / nbx) * by + y - halo;
unsigned int gx, gy;
block_global_xy(x, y, halo, d_block_channel.nx, gx, gy);
const unsigned long base = (unsigned long)blockIdx.z * NQ * TOTAL_CELLS;
const unsigned long cell = (unsigned long)blockIdx.z * TOTAL_CELLS + k;
float f[NQ];
@@ -55,11 +53,7 @@ extern "C" __global__ void BlockChannelStep(
}
if (!wall && !outlet) {
#if COLLISION_MODEL == 2
// Match uniform MRT arithmetic (collide_dispatch, zero forcing).
float rho, ux, uy;
compute_rho_u(f, rho, ux, uy);
collide_mrt_no_force(f, rho, ux, uy,
fminf(OMEGA_COLLISION_MAX, fmaxf(OMEGA_COLLISION_MIN, d_params.omega)));
collide_mrt_unforced(f);
#else
// Match uniform SRT arithmetic, including its shifted equilibrium path.
float rho, ux, uy, feq[NQ], forcing[NQ] = {};
+17 -8
View File
@@ -336,13 +336,19 @@ class Simulation:
def read_surface_exchange(self, id: int):
"""Latest step's wall/aperture (Fx,Fy,Tz) exchange, not total nozzle force.
Supports SurfaceActuation and Jet-driven bodies, including zero-amplitude
apertures. Passive bodies without an aperture are rejected.
Unlike read_body this is not accumulated/time-averaged. It resets after
geometry sync or checkpoint load; advance before interpreting it.
"""
if self.bodies.get(id).surface_actuation is None:
obj = self.bodies.get(id)
curved = self.field.curved
has_aperture = (curved.aperture is not None
and np.any(curved.aperture & (curved.body_id == id)))
if obj.surface_actuation is None and not has_aperture:
raise ValueError("Body has no surface actuation")
self.stream.synchronize()
return self.field.curved.surface_exchange(id)
return curved.surface_exchange(id)
@context_bound
def read_body(self, id: int, *,
@@ -451,18 +457,21 @@ class Simulation:
@context_bound
def initialize(self):
"""Initialize flow field and sync objects to GPU."""
# Recompile if objects were added after construction.
self._assert_allocation_contract()
# Validate the complete geometry before flags, populations or modules
# change. Compact-list construction publishes no outputs on failure.
next_flags = self.bodies.build_flags(self.field.build_channel_flags())
if self.bodies.jets and self.bodies.count == 0:
raise ValueError("Jets need bodies with cut links")
self.bodies.build_compact_lists_for(self.bodies.objects, next_flags)
# Recompile if objects were added after construction.
if self._read_generated_n_objects() != self.bodies.count:
self.recompile()
self.field.flag = self.field.build_channel_flags()
if self.bodies.count > 0:
self.field.flag = self.bodies.build_flags(self.field.flag)
self.field.flag = next_flags
self.field.upload_flags()
if self.bodies.jets and self.bodies.count == 0:
raise ValueError("Jets need bodies with cut links")
self.stepper.initialize()
if self.bodies.count > 0:
self.bodies.sync_to_gpu(self.field, rebuild_flags=False)
+79
View File
@@ -0,0 +1,79 @@
"""CPU-only contract tests for run_dfg_re20. Not CUDA or DFG acceptance evidence."""
import sys
from pathlib import Path
import unittest
sys.path.insert(0, str(Path(__file__).resolve().parents[1] / "validation"))
import run_dfg_re20 as v # noqa: E402
import run_refined_dfg as rr # noqa: E402
h, _ = rr.helpers(rr.DEFAULT_SOURCE)
def rows(values, tstar_end=v.TSTAR_MAX):
n = int(round(tstar_end / v.SAMPLE_TSTAR))
return [dict(tstar=(i + 1) * v.SAMPLE_TSTAR, **values(i)) for i in range(n)]
class Re20Contract(unittest.TestCase):
def test_lattice_parameters_and_bounds(self):
root, uniform = v.lattice_parameters(40), v.lattice_parameters(80)
self.assertAlmostEqual(root["tau"], 0.56, places=12)
self.assertAlmostEqual(uniform["tau"], 0.62, places=12)
self.assertEqual((root["steps"], root["interval"]), (240000, 2000))
self.assertEqual((uniform["steps"], uniform["interval"]), (480000, 4000))
self.assertAlmostEqual(v.plan()["refined_fine_tau"], 0.62, places=12)
def test_config_only_changes_viscosity(self):
base = v._re100_config(h, 40, "SRT", "none")
cfg, body, p = v.config(h, 40, "SRT")
self.assertAlmostEqual(cfg["physics"]["viscosity"], 0.01 * 40 / 20, places=15)
self.assertEqual((p["re"], p["viscosity"]), (20.0, cfg["physics"]["viscosity"]))
base[0]["physics"]["viscosity"] = cfg["physics"]["viscosity"]
self.assertEqual(base[0], cfg)
self.assertEqual(base[1], body)
with self.assertRaisesRegex(ValueError, "no Jets"):
v.config(h, 40, "MRT", "zero")
def test_units(self):
s = v.sample([2.0, -0.5], 4, 40, 3.0)
den = rr.SPEED**2 * 40 / 2
self.assertAlmostEqual(s["cd"], 2.0 / 4 / den)
self.assertAlmostEqual(s["cl"], -0.5 / 4 / den)
self.assertAlmostEqual(s["p_diff"], 3.0 * 0.04)
self.assertEqual(s["dp_scaled"], 3.0)
def test_steady_and_verdict(self):
inside = dict(cd=5.58, cl=0.0106, p_diff=0.1174)
out = v.summarize(rows(lambda i: inside))
self.assertEqual((out["status"], out["steady"], out["window_samples"]),
("WITHIN_INTERVALS", True, 21))
self.assertTrue(out["cd_positive"])
self.assertAlmostEqual(out["edge_distance"]["cl"], 0.0002)
self.assertTrue(all(out["verdict"].values()))
low = v.summarize(rows(lambda i: dict(inside, cl=0.0100)))
self.assertEqual(low["status"], "OUTSIDE_INTERVALS")
self.assertFalse(low["verdict"]["cl"])
def test_slow_drift_gives_no_verdict(self):
# Range 2e-5 passes (limit 6e-5); slope * window 2e-5 exceeds 1.2e-5.
out = v.summarize(rows(lambda i: dict(cd=5.58, cl=0.0106 + 1e-6 * i, p_diff=0.1174)))
self.assertEqual((out["status"], out["verdict"]), ("NOT_STEADY", None))
self.assertLessEqual(out["ranges"]["cl"], out["range_limits"]["cl"])
self.assertGreater(out["drifts"]["cl"], out["slope_limits"]["cl"])
def test_noise_range(self):
quiet = v.summarize(rows(lambda i: dict(cd=5.58, cl=0.0106 + 2e-5 * (i % 2), p_diff=0.1174)))
self.assertTrue(quiet["steady"]) # within the range limit, no trend
noisy = v.summarize(rows(lambda i: dict(cd=5.58, cl=0.0106 + 1e-4 * (i % 2), p_diff=0.1174)))
self.assertEqual(noisy["status"], "NOT_STEADY")
self.assertGreater(noisy["ranges"]["cl"], noisy["range_limits"]["cl"])
def test_incomplete_run_gives_no_verdict(self):
out = v.summarize(rows(lambda i: dict(cd=5.58, cl=0.0106, p_diff=0.1174), tstar_end=30))
self.assertEqual((out["status"], out["verdict"]), ("INCOMPLETE", None))
if __name__ == "__main__":
unittest.main()
+34
View File
@@ -16,6 +16,7 @@ from run_jet_circle_cv import (
case,
state,
cv,
cv_from_macros,
aperture_probe,
measured_aperture_flux,
verify,
@@ -28,6 +29,39 @@ def eq(rho, u, v):
class Host(unittest.TestCase):
def test_public_macros_pressure_advection_and_cropped_frames(self):
for h, origin, shape, rect in (
(.5, (0., 0.), (48, 64), (5., 4., 25., 20.)),
(.5, (.25, .5), (48, 64), (5.25, 4., 25.25, 20.)),
(.25, (.375, .75), (96, 128), (5.125, 4., 25.125, 20.)),
):
y, x = np.indices(shape)
x = origin[0] + h * (x + .5)
k, u, v = 1e-5, .02, -.01
rho = 1 + 3 * k * x # p=(rho-1)/3=k*x
ux, uy, fluid = np.full(shape, u), np.full(shape, v), np.ones(shape, bool)
result = cv_from_macros(rho, ux, uy, fluid, origin, rect, .004, h)
expected = 320 * np.array([3*k*u, k + 3*k*u*u, 3*k*u*v])
np.testing.assert_allclose(result[1], expected, rtol=1e-11, atol=1e-13)
np.testing.assert_allclose(result, cv(eq(rho, u, v), fluid, origin, rect, .004, h), atol=1e-12)
x0, y0, x1, y1 = np.rint((np.array(rect)-np.tile(origin, 2))/h).astype(int)
selection = np.s_[y0-2:y1+2, x0-2:x1+2]
cropped_origin = np.asarray(origin) + h*np.array([x0-2, y0-2])
cropped = cv_from_macros(rho[selection], ux[selection], uy[selection],
fluid[selection], cropped_origin, rect, .004, h)
np.testing.assert_array_equal(cropped, result)
def test_public_macros_full_normal_viscous_stress(self):
y, x = np.indices((48, 64))
x = (x + .5) * .5
rho, ux, uy, fluid = np.ones_like(x), 1e-4*x*x, np.zeros_like(x), np.ones(x.shape, bool)
args = (rho, ux, uy, fluid, (0., 0.), (5., 4., 25., 20.))
_, viscous = cv_from_macros(*args, .004)
_, inviscid = cv_from_macros(*args, 0.)
np.testing.assert_allclose(viscous-inviscid, [0, -4*.004*1e-4*320, 0], atol=1e-13)
with self.assertRaisesRegex(ValueError, "matching 2D"):
cv_from_macros(rho, ux, uy[:-1], fluid, (0, 0), (5, 4, 25, 20), .004)
def test_descriptor_and_uniform_closed_flux(self):
from CelerisLab.lbm.descriptors import D2Q9_EX, D2Q9_EY
+49
View File
@@ -188,6 +188,55 @@ def jet_case(device, jets):
return field, bodies
def test_public_surface_exchange_for_jet_preserves_aperture_at_zero_and_reverse(device):
from CelerisLab.simulation import Simulation
jet = Jet(Sector(CENTER, 0., .6, 3.), Radial(CENTER, inward=False), "quartic", 2e-3)
field, bodies = jet_case(device, [jet])
sim = SimpleNamespace(bodies=bodies, field=field, _initialized=True,
stream=SimpleNamespace(synchronize=device.synchronize))
cl = field.curved
assert bodies.get(0).surface_actuation is None
aperture, velocity = cl.aperture, cl.surface_velocity.copy()
assert aperture.any() and (~aperture).any()
# Synthetic per-link exchanges test readback/splitting, not kernel physics.
values = np.arange(cl.count * 3, dtype=np.float32).reshape(-1, 3)
device.htod(cl.link_exchange_gpu, values)
for amplitude in (2e-3, 0., -1e-3):
Simulation.set_jet_amplitude(sim, 0, amplitude)
result = Simulation.read_surface_exchange(sim, 0)
assert cl.aperture is aperture
np.testing.assert_array_equal(aperture, cl.jet_id >= 0)
np.testing.assert_allclose(cl.surface_velocity, velocity * (amplitude / 2e-3))
for name, mask in (("wall", ~aperture), ("aperture", aperture)):
np.testing.assert_array_equal(result[name], values[mask].sum(axis=0, dtype=np.float64))
def test_public_surface_exchange_keeps_legacy_and_passive_guards(device):
from CelerisLab.simulation import Simulation
field = make_field(device)
bodies = manager(field, [circle(SurfaceActuation(0., .6, .002), radius=2.)])
bodies.sync_to_gpu(field)
sim = SimpleNamespace(bodies=bodies, field=field,
stream=SimpleNamespace(synchronize=device.synchronize))
for value in Simulation.read_surface_exchange(sim, 0).values():
np.testing.assert_array_equal(value, 0.)
field.curved.free_gpu_columns()
with pytest.raises(RuntimeError, match="diagnostic is allocated"):
Simulation.read_surface_exchange(sim, 0)
# An exchange buffer elsewhere in the scene must not admit a passive body.
for jets in ([], [Jet(Sector(CENTER, 0., .6, 3.), Radial(CENTER))]):
field, bodies = jet_case(device, jets)
passive = bodies.add(circle(center=(2., 3.), radius=.6))
bodies.sync_to_gpu(field)
sim.bodies, sim.field = bodies, field
with pytest.raises(ValueError, match="Body has no surface actuation"):
Simulation.read_surface_exchange(sim, passive)
if not jets:
with pytest.raises(ValueError, match="Body has no surface actuation"):
Simulation.read_surface_exchange(sim, 0)
def test_manager_passes_true_hits_and_reuploads_only_velocity(device):
# CPU memory double only: checks host/device bookkeeping, not GPU numerics.
jet = Jet(Sector(CENTER, 0., .6, 3.), Radial(CENTER, inward=False), "quartic", 2e-3)
+174 -4
View File
@@ -146,23 +146,26 @@ def test_full_requires_completed_pilot():
r.verify_pilot(None, r.verify_source(r.DEFAULT_SOURCE, "MRT", "window"))
def pilot_fixture(path, observation_mode="window"):
def pilot_fixture(path, observation_mode="window", jet_scenario="none", case_selection="both", uniform_diameter=80, placement="wide"):
"""Synthetic contract fixture only; never a physical result or run receipt."""
manifest = (r.verify_source(r.DEFAULT_SOURCE, "MRT", "window")
manifest = (r.verify_source(r.DEFAULT_SOURCE, "MRT", "window", jet_scenario)
if observation_mode == "window" else
json.loads((r.HERE / "data/refined_dfg/source_manifest_mrt.json").read_text()))
selection = dict(case_selection=case_selection, uniform_diameter=uniform_diameter, placement=placement)
(path / "plan.json").write_text(
json.dumps(
dict(
source_manifest=manifest,
**selection,
collision="MRT",
jet_scenario=jet_scenario,
observation_mode=observation_mode,
bounds_root_edge=list(r.BOUNDS),
bounds_root_edge=list(r.PLACEMENTS[placement]),
runner_sha256=r.runner_hash(),
)
)
)
for case, diameter in (("uniform", 80), ("refined", 40)):
for case, diameter in r.selected_cases(case_selection, uniform_diameter):
dest = path / case
dest.mkdir()
interval = round(0.02 * diameter / r.SPEED)
@@ -189,7 +192,9 @@ def pilot_fixture(path, observation_mode="window"):
json.dumps(
dict(
case=case,
**selection,
collision="MRT",
jet_scenario=jet_scenario,
observation_mode=observation_mode,
mode="pilot",
status="pilot_complete",
@@ -206,7 +211,9 @@ def pilot_fixture(path, observation_mode="window"):
json.dumps(
dict(
case=case,
**selection,
collision="MRT",
jet_scenario=jet_scenario,
observation_mode=observation_mode,
mode="pilot",
step=interval,
@@ -451,6 +458,169 @@ def test_window_contract_rejection():
assert not backend.events
def test_public_jet_configuration_and_geometry():
for diameter, center, radius in ((40, (80.5, 81), 20), (80, (160, 160.5), 40)):
cfg, _, _ = r.config(h, diameter, "MRT", "fixed")
assert not cfg["method"]["ddf_shifting"] and not cfg["method"]["les"]["enabled"]
jets = r.public_jets(center, radius, "fixed")
assert [j.amplitude for j in jets] == [.001, -.001]
assert all(j.field.inward is False and j.profile == "parabolic" for j in jets)
assert all(j.region.r_max == radius * 1.005 for j in jets)
assert all(j.amplitude == 0 for j in r.public_jets(center, radius, "zero"))
cfg, _, _, host = r.host_geometry(r.DEFAULT_SOURCE, h, "MRT", "fixed")
assert not cfg.ddf_shifting and len(host.boundary_cells) > 0
assert r.public_jets((0, 0), 1, "none") == ()
with unittest.TestCase().assertRaises(ValueError):
r.config(h, 40, "SRT", "fixed")
def test_public_jet_reversal_boundary_and_windows():
from types import SimpleNamespace
calls = []
handle = SimpleNamespace(set_jet_amplitude=lambda i, a: calls.append((i, a)))
for diameter in (40, 80):
boundary = round(250 * diameter / r.SPEED)
assert r.jet_interval(handle, "fixed", boundary - 3, 80, diameter) == (3, None)
switch = round(300 * diameter / r.SPEED)
assert r.jet_interval(handle, "reverse", switch - 3, 80, diameter) == (3, None)
assert not calls
n, event = r.jet_interval(handle, "reverse", switch, 80, diameter)
assert n == 80 and event["step"] == switch and event["tstar"] == 300
assert calls == [(0, -.001), (1, .001)]
calls.clear()
assert r.jet_interval(handle, "reverse", switch + 80, 80, diameter) == (80, None)
assert r.jet_interval(handle, "fixed", switch, 80, diameter) == (80, None)
assert not calls
rows = [dict(tstar=t, tstar_force=t - .5, cd=2.0, cl=-.1) for t in range(251, 306)]
windows = r.jet_diagnostics(rows, "reverse")
assert len(windows) == 6 and all(w["complete"] for w in windows)
assert all(w["cd"]["mean"] == 2 and np.isclose(w["cl"]["mean"], -.1) for w in windows)
assert windows[-1]["covered_tstar"] == 5
with unittest.TestCase().assertRaisesRegex(ValueError, "crosses"):
r.jet_diagnostics([dict(tstar=250.5, tstar_force=250, cd=1, cl=0)], "fixed")
assert r.plan(h, "MRT", "window", "reverse")["modes"]["full_tstar"] == 305
def test_public_jet_source_and_pilot_separation():
from tempfile import TemporaryDirectory
with TemporaryDirectory() as tmp:
path = Path(tmp)
manifest = pilot_fixture(path, jet_scenario="fixed")
assert manifest["source_capture"].startswith("current checkout")
assert len(manifest["checkout_revision"]) == 40
assert r.verify_pilot(path, manifest, "MRT", "window", "fixed") == 3606.0
for scenario in ("none", "zero", "reverse"):
with unittest.TestCase().assertRaisesRegex(ValueError, "Jet scenario"):
r.verify_pilot(path, manifest, "MRT", "window", scenario)
for relative in ("uniform/summary.json", "refined/ready.json"):
receipt = path / relative
record = json.loads(receipt.read_text())
receipt.write_text(json.dumps(dict(record, jet_scenario="zero")))
with unittest.TestCase().assertRaises(ValueError):
r.verify_pilot(path, manifest, "MRT", "window", "fixed")
receipt.write_text(json.dumps(record))
with unittest.TestCase().assertRaises(ValueError):
r.verify_source(r.DEFAULT_SOURCE, "MRT", "last_base_step", "fixed")
def test_cv_snapshot_common_units_and_window_endpoints():
records = []
for refined, shape, origin, diameter, impulse in (
(True, (240, 568), (38., 22.), 40, [4., -8.]),
(False, (330, 1761), (.25, .5), 80, [16., -32.]),
(False, (658, 3521), (.375, .75), 160, [64., -128.]),
):
rho, ux, uy, fluid = np.ones(shape), np.full(shape, .01), np.zeros(shape), np.ones(shape, bool)
begin, n = round(290*diameter/r.SPEED), round(.02*diameter/r.SPEED)
record = r.cv_snapshot(rho, ux, uy, fluid, origin, refined, begin, n, diameter, impulse)
records.append(record)
np.testing.assert_allclose(record["outward_flux"], 0, atol=1e-12)
assert r.cv_selected(begin, diameter, "full") and not r.cv_selected(begin-n, diameter, "full")
end = round(300*diameter/r.SPEED)
assert r.cv_selected(end, diameter, "full") and not r.cv_selected(end+n, diameter, "full")
assert r.cv_selected(n, diameter, "pilot")
assert sum(r.cv_selected(step, diameter, "full") for step in range(begin-n, end+n+1, n)) == 501
for key in ("time_root", "interval_start_root", "interval_dt_root", "interval_impulse_root", "inventory"):
for record in records[1:]:
np.testing.assert_allclose(records[0][key], record[key], rtol=0, atol=1e-10)
assert records[0]["interval_dt_root"] == 80 and np.isclose(records[0]["tstar"], 290.02)
np.testing.assert_array_equal(records[0]["interval_impulse_root"], [4, -8])
def test_cv_pilot_mode_and_helper_provenance():
from tempfile import TemporaryDirectory
manifest = r.verify_source(r.DEFAULT_SOURCE, "MRT", "window", "fixed", True)
assert "tests/validation/run_jet_circle_cv.py" in manifest["sha256"]
with TemporaryDirectory() as tmp:
path = Path(tmp)
old = pilot_fixture(path, jet_scenario="fixed")
with unittest.TestCase().assertRaisesRegex(ValueError, "CV observation mode"):
r.verify_pilot(path, old, "MRT", "window", "fixed", True)
for relative in ("plan.json", "uniform/summary.json", "refined/summary.json",
"uniform/ready.json", "refined/ready.json"):
file = path / relative
record = json.loads(file.read_text())
record.update(observe_cv=True, cv_samples=250)
if relative == "plan.json":
record["source_manifest"] = manifest
file.write_text(json.dumps(record))
assert r.verify_pilot(path, manifest, "MRT", "window", "fixed", True) == 3606
def test_compact_geometry_and_cv_stencils():
from CelerisLab.lbm.refinement import ACTIVE
from CelerisLab.lbm.descriptors import SOLID
_, pair, _, host = r.host_geometry(r.DEFAULT_SOURCE, h, "MRT", "fixed", "compact")
assert pair.fine_shape == (168, 168) and tuple(pair.fine_origin) == (46, 46)
fluid = (pair.fine_kind == ACTIVE) & ((host.flags.reshape(pair.fine_shape) & SOLID) == 0)
rho, ux, uy = np.ones(pair.fine_shape), np.full(pair.fine_shape, .01), np.zeros(pair.fine_shape)
record = r.cv_snapshot(rho, ux, uy, fluid, pair.fine_origin, True, 1160000, 80, 40, [1, 2], "compact")
np.testing.assert_allclose(record["outward_flux"], 0, atol=1e-12)
stencil = np.zeros(pair.fine_shape, bool)
for rect in r.cv_contours(True, 40, "compact"):
x0, y0, x1, y1 = np.rint((rect - np.tile(pair.fine_origin, 2))/.5).astype(int)
stencil[y0-2:y1+2, x0-2:x0+2] = stencil[y0-2:y1+2, x1-2:x1+2] = True
stencil[y0-2:y0+2, x0-2:x1+2] = stencil[y1-2:y1+2, x0-2:x1+2] = True
assert fluid[stencil].all() and not stencil.ravel()[host.transfer_fine_cells].any()
def test_d160_config_and_single_case_receipts():
from tempfile import TemporaryDirectory
from unittest.mock import patch
cfg, _, p = r.config(h, 160, "MRT", "fixed")
assert (p["nx"], p["ny"], p["center"], p["radius"]) == (3521, 658, [320, 320.5], 80)
assert p["viscosity"] == .016 and p["mean_speed"] == .01 and not cfg["method"]["ddf_shifting"]
assert r.uniform_origin(160) == (.375, .75)
np.testing.assert_array_equal(r.cv_contours(False, 160), r.CV_CONTOURS + [.125, 0, .125, 0])
for scenario, expected_exit in (("fixed", 0), ("zero", 2)):
with TemporaryDirectory() as tmp:
path = Path(tmp)
manifest = pilot_fixture(path, jet_scenario=scenario, case_selection="uniform", uniform_diameter=160)
assert r.verify_pilot(path, manifest, "MRT", "window", scenario, False, "uniform", 160) == 1803
for selection, diameter, placement in (("both", 160, "wide"), ("uniform", 80, "wide"), ("uniform", 160, "compact")):
with unittest.TestCase().assertRaises(ValueError):
r.verify_pilot(path, manifest, "MRT", "window", scenario, False, selection, diameter, placement)
# Synthetic dispatch/result check: no CUDA imports or execution.
output = path / "full"
argv = ["runner", "--collision", "MRT", "--exchange-window", "--jet-scenario", scenario,
"--case", "uniform", "--uniform-diameter", "160", "--mode", "full",
"--pilot-results", str(path), "--output", str(output), "--max-wall-seconds", "10", "--gpu-gates-approved"]
result = dict(case="uniform", healthy=True, periodic=scenario == "zero", jet_diagnostic_windows=[],
status="driven_diagnostics_complete" if scenario == "fixed" else "periodic",
reference_comparison=dict(reference_agreement=False))
with patch.object(sys, "argv", argv), patch.dict(r.os.environ, CUDA_VISIBLE_DEVICES="mock-no-gpu"), \
patch.object(r, "run_case", return_value=result) as run:
assert r.main() == expected_exit and run.call_count == 1
comparison = json.loads((output / "comparison.json").read_text())
assert comparison["matched_case_pass"] is False and "refined_vs_uniform" not in comparison
assert comparison["status"].startswith("single_case_")
if __name__ == "__main__":
suite = unittest.TestSuite(
unittest.FunctionTestCase(fn)
+6 -1
View File
@@ -37,8 +37,13 @@ class RefinementMRTHost(unittest.TestCase):
self.assertIn("STORE_PRECISION != 0", source)
self.assertIn('#if COLLISION_MODEL == 2\n#include "operators/collision_mrt.cuh"\n#endif', source)
self.assertIn("USE_DDF_SHIFTING ||", refinement) # dense/mixed shifted stays rejected
# One shared unforced MRT body; each blocked/patch path calls it exactly once.
mrt = (KERNELS / "operators/collision_mrt.cuh").read_text()
self.assertEqual(mrt.count("void collide_mrt_unforced("), 1)
for source in (blocks, channel, refinement):
self.assertEqual(source.count("collide_mrt_no_force("), 1)
self.assertEqual(source.count("collide_mrt_unforced(f);"), 1)
self.assertNotIn("collide_mrt_no_force(", source)
self.assertNotIn("compute_rho_u(f, rho, ux, uy);\n collide_mrt", source)
if __name__ == "__main__": unittest.main()
+75
View File
@@ -238,6 +238,81 @@ def test_overlapping_force_regions_rejected(device):
bodies.build_compact_lists(bodies.build_flags(field.flag))
@pytest.mark.parametrize("second_x,error", [(14., "unique cut-link writers"),
(17., "active fluid receivers")])
def test_passive_overlap_rejected_before_publishing_lists(second_x, error):
cfg = LBMConfig(nx=32, ny=24)
cfg.validate()
bodies = ObjectManager(cfg.nx, cfg.ny, cfg.nz, cfg.nq, cfg)
for x in (14., second_x):
bodies.add(obj(x=x, y=12., r=4.3))
bodies.add(obj(x=4., y=4., r=2., is_sensor=True))
counts = np.full(bodies.count, 91, np.int32)
hits = []
flags = bodies.build_flags(np.full(cfg.nx * cfg.ny, FLUID, np.uint16))
for domain_flags in (flags, None):
with pytest.raises(ValueError, match=error):
bodies.build_compact_lists_for(bodies.objects, domain_flags,
sensor_cell_counts_out=counts, hits_out=hits)
np.testing.assert_array_equal(counts, 91)
assert hits == []
@pytest.mark.parametrize("centers", [((10., 12.), (22., 12.)),
((10.5, 12.), (19.5, 12.))])
def test_separated_passive_bodies_keep_valid_writers(centers):
# The second case has a subcell physical gap with a resolved fluid column.
cfg = LBMConfig(nx=32, ny=24)
cfg.validate()
bodies = ObjectManager(cfg.nx, cfg.ny, cfg.nz, cfg.nq, cfg)
for x, y in centers:
bodies.add(obj(x=x, y=y, r=4.3))
flags = bodies.build_flags(np.full(cfg.nx * cfg.ny, FLUID, np.uint16))
indices, directions, _, ids, *_ = bodies.build_compact_lists(flags)
assert set(ids) == {0, 1}
assert np.all(flags[indices] & FLUID) and not np.any(flags[indices] & SOLID)
assert len(np.unique(indices.astype(np.uint64) * cfg.nq + directions)) == len(indices)
@pytest.mark.parametrize("entry", ["sync", "initialize", "runtime_edit"])
@pytest.mark.parametrize("second_x", [5., 6.])
def test_passive_overlap_failure_keeps_live_state(device, entry, second_x):
from CelerisLab.simulation import Simulation
field = make_field(device)
bodies = manager(field, [obj(), obj(x=9., y=3., r=1., is_sensor=True)])
bodies.sync_to_gpu(field)
overlapping = obj(x=second_x)
if entry == "runtime_edit":
bodies.stage_add(overlapping)
else:
bodies.add(overlapping)
objects = bodies.objects
flags, curved, counts = field.flag.copy(), field.curved.fluid_idx.copy(), bodies.sensor_cell_counts.copy()
action = bodies.action.copy()
buffers = [(block, bytes(block.data), block.freed) for block in device.blocks]
writes = device.writes
sim = SimpleNamespace(bodies=bodies, field=field, lbm_cfg=field.cfg,
_initialized=entry == "runtime_edit",
_assert_allocation_contract=lambda: None,
stream=SimpleNamespace(synchronize=device.synchronize))
with pytest.raises(ValueError, match="active fluid receivers|unique cut-link writers"):
if entry == "sync":
bodies.sync_to_gpu(field)
elif entry == "initialize":
Simulation.initialize(sim)
else:
Simulation.sync_bodies(sim)
assert bodies.objects == objects
assert bodies.has_pending_edit() == (entry == "runtime_edit")
assert sim._initialized == (entry == "runtime_edit")
assert device.writes == writes and len(device.blocks) == len(buffers)
assert all(bytes(block.data) == data and block.freed == freed for block, data, freed in buffers)
np.testing.assert_array_equal(field.flag, flags)
np.testing.assert_array_equal(field.curved.fluid_idx, curved)
np.testing.assert_array_equal(bodies.sensor_cell_counts, counts)
np.testing.assert_array_equal(bodies.action, action)
def test_action_upload_and_scratch_are_pinned(device):
field = make_field(device, streaming="esopull")
bodies = manager(field, [obj(is_force_region=True)])
@@ -80,11 +80,12 @@ class ThreeLevelCPU(unittest.TestCase):
f, g = run._levels[1:]
b = g.boundary
events, feeds = [], []
advance, gather = run._advance_child, run._gather_halo
def record_feed(buffer, **kw):
self.assertIs(buffer, (f.current, f.spare)[len(feeds)])
feeds.append(buffer)
advance(buffer, **kw)
advance, gather = run._advance, run._gather_halo
def record_feed(index, buffer, **kw): # index 2: L1 hop feeds L2
if index == 2:
self.assertIs(buffer, (f.current, f.spare)[len(feeds)])
feeds.append(buffer)
advance(index, buffer, **kw)
def record_halo(level, buffer, **kw):
if level is g:
events.append(("halo", buffer))
@@ -95,7 +96,7 @@ class ThreeLevelCPU(unittest.TestCase):
self.assertIs(kind, g.kind)
events.append(("step", src))
g.kernel.side_effect = record_step
with patch.object(run, "_advance_child", side_effect=record_feed), \
with patch.object(run, "_advance", side_effect=record_feed), \
patch.object(run, "_gather_halo", side_effect=record_halo):
run.step()
self.assertEqual(feeds, [f.current, f.spare])
@@ -105,8 +106,8 @@ class ThreeLevelCPU(unittest.TestCase):
self.assertGreater(len(np.unique(b.tables["block"])), 1)
# Negative control: reusing L1's old source at the midpoint must fail.
feeds.clear()
with patch.object(run, "_advance_child", side_effect=lambda buffer, **kw:
record_feed(f.current, **kw)):
with patch.object(run, "_advance", side_effect=lambda index, buffer, **kw:
record_feed(index, f.current if index == 2 else buffer, **kw)):
with self.assertRaises(AssertionError):
run.step()
run.close()
@@ -172,11 +173,12 @@ class ThreeLevelGPU(unittest.TestCase):
p1, p2 = run.patch, run.child_patch
run.initialize(state(16, 16, 1), state(*p1.fine_shape, 2), state(*p2.fine_shape, 3))
f = run._levels[1]
feeds, original = [], run._advance_child
def record(buffer, **kw):
feeds.append(int(buffer))
original(buffer, **kw)
with patch.object(run, "_advance_child", side_effect=record):
feeds, original = [], run._advance
def record(index, buffer, **kw): # index 2: L1 hop feeds L2
if index == 2:
feeds.append(int(buffer))
original(index, buffer, **kw)
with patch.object(run, "_advance", side_effect=record):
cur, spare = int(f.current), int(f.spare)
run.step(1)
self.assertEqual(feeds, [cur, spare]) # current G, then the new G of hop 1
+222
View File
@@ -0,0 +1,222 @@
"""Steady DFG 2D-1 (Re 20): refined and uniform runs against the official reference intervals.
Not a full benchmark certification. Declared deviations from the official setup:
pressure-NEQ outlet (``neq_extrap``) instead of do-nothing, local Zou-He inlet.
Geometry, inflow profile, initial state, refined layout and observation reuse the
pinned Re100 runner (``run_refined_dfg``) and ``re100_helpers`` unchanged; only the
lattice viscosity is set for Re 20 (nu = U_lattice * D / 20 at the root level).
Units. The helpers use scaled DFG units with mean inflow speed 1, so
Cd = 2 Fx / (rho U^2 D) and Cl = 2 Fy / (rho U^2 D) are scale-free, and
``pressure_probes`` returns dp / (rho U^2). The official p_diff = p(0.15, 0.2) -
p(0.25, 0.2) uses U = 0.2 m/s, rho = 1, so p_diff = dp * 0.04. Both are reported;
only p_diff is compared with the official interval. Forces use the existing sign
convention: F is the force of the fluid on the cylinder, i.e. the refined raw
exchange impulse (window ledger, ``total.impulse``) or the uniform ``read_force``,
with x along the inflow and y up from the bottom wall. Cd must be positive, and the
official Cl is positive (centre 0.20 below the centreline 0.205), so a flipped sign
shows up as Cl outside its interval.
Sampling. One sample every SAMPLE_TSTAR (t* = U t / D; 0.25 s), taken at the end of
a completed root step with all levels synchronized; the step index is recorded. Cd
and Cl are means over the sample interval (window exchange ledger refined, per-batch
forces uniform), which filters acoustic and step-parity oscillation; p_diff is the
end-of-interval value at the exact surface points.
Steady rule (our engineering choice, frozen before any run; not official). Over the
trailing WINDOW_TSTAR (t* 50..60 inclusive, 21 samples), for each of Cd, Cl and
p_diff: range (max - min) <= 10 % and |least-squares slope * window| <= 2 % of the
width of its official interval. Absolute limits, so the small Cl is never a divisor;
the slope term bounds slow monotone drift that the range alone would pass. If the
rule fails at TSTAR_MAX the run reports "not steady" and gives no interval verdict;
limits are never relaxed after a run. The verdict uses the window mean, and the
distance of each mean to its nearest interval edge is reported (negative outside).
"""
import argparse
import json
import math
import os
from pathlib import Path
import sys
import time
from tempfile import TemporaryDirectory
import numpy as np
HERE = Path(__file__).resolve().parent
sys.path.insert(0, str(HERE))
import run_refined_dfg as rr # noqa: E402
RE = 20.0
U_PHYS = 0.2 # m/s mean inflow; rho = 1
TSTAR_MAX = 60.0 # 30 s physical
SAMPLE_TSTAR = 0.5 # 0.25 s
WINDOW_TSTAR = 10.0 # trailing 5 s, 21 samples
# Schaefer & Turek (1996), 2D-1 lower/upper bounds.
BANDS = dict(cd=(5.57, 5.59), cl=(0.0104, 0.0110), p_diff=(0.1172, 0.1176))
STEADY_RANGE = {k: (hi - lo) / 10 for k, (lo, hi) in BANDS.items()}
STEADY_SLOPE = {k: (hi - lo) / 50 for k, (lo, hi) in BANDS.items()}
DEVIATIONS = ("pressure-NEQ outlet (neq_extrap), not do-nothing", "local Zou-He inlet")
_re100_config = rr.config
def config(h, diameter, collision="SRT", jet_scenario="none"):
"""The pinned Re100 configuration with the lattice viscosity set for Re 20."""
if jet_scenario != "none":
raise ValueError("DFG 2D-1 runs have no Jets")
cfg, body, p = _re100_config(h, diameter, collision, jet_scenario)
nu = p["mean_speed"] * p["diameter"] / RE
cfg["physics"]["viscosity"] = nu
return cfg, body, dict(p, viscosity=nu, re=RE)
def lattice_parameters(diameter, speed=rr.SPEED):
nu = speed * diameter / RE
return dict(viscosity=nu, tau=0.5 + 3 * nu, steps=math.ceil(TSTAR_MAX * diameter / speed),
interval=round(SAMPLE_TSTAR * diameter / speed))
def sample(impulse, n, diameter, dp):
den = rr.SPEED**2 * diameter / 2
return dict(cd=float(impulse[0] / n / den), cl=float(impulse[1] / n / den),
dp_scaled=float(dp), p_diff=float(dp) * U_PHYS**2)
def summarize(rows):
"""Steady rule over the trailing window, then the interval verdict (or none)."""
if not rows or rows[-1]["tstar"] < TSTAR_MAX - 1e-9:
return dict(status="INCOMPLETE", steady=False, verdict=None)
window = [r for r in rows if r["tstar"] >= TSTAR_MAX - WINDOW_TSTAR - 1e-9]
t = np.array([r["tstar"] for r in window])
ranges = {k: max(r[k] for r in window) - min(r[k] for r in window) for k in BANDS}
drifts = {k: abs(np.polyfit(t, [r[k] for r in window], 1)[0]) * WINDOW_TSTAR for k in BANDS}
steady = all(ranges[k] <= STEADY_RANGE[k] and drifts[k] <= STEADY_SLOPE[k] for k in BANDS)
final = {k: float(np.mean([r[k] for r in window])) for k in BANDS}
edge = {k: min(final[k] - BANDS[k][0], BANDS[k][1] - final[k]) for k in BANDS}
result = dict(window_samples=len(window), ranges=ranges, drifts=drifts,
range_limits=STEADY_RANGE, slope_limits=STEADY_SLOPE, steady=steady,
window_mean=final, edge_distance=edge, bands=BANDS,
deviations=DEVIATIONS, cd_positive=final["cd"] > 0)
if not steady:
return dict(result, status="NOT_STEADY", verdict=None)
inside = {k: BANDS[k][0] <= final[k] <= BANDS[k][1] for k in BANDS}
return dict(result, status="WITHIN_INTERVALS" if all(inside.values()) else "OUTSIDE_INTERVALS",
verdict=inside)
def healthy(row):
return row["max_mach"] <= 0.2 and row["rho_min"] >= 0.5 and row["rho_max"] <= 1.5
def run_case(a, h, case):
from contextlib import ExitStack
from CelerisLab.cuda.context import CudaContext
from CelerisLab.lbm.descriptors import FLUID
from CelerisLab.lbm.refinement_stepper import FixedPatchStepper
from CelerisLab.simulation import Simulation
refined = case == "refined"
cfgdict, bodydict, p = config(h, 40 if refined else 80, a.collision)
lp = lattice_parameters(p["diameter"])
rows = []
with ExitStack() as stack:
if refined:
cfg, pair, body, host = rr.host_geometry(a.source, h, a.collision)
context = stack.enter_context(CudaContext(0))
backend = stack.enter_context(FixedPatchStepper(
cfg, rr.PLACEMENTS["wide"], context=context, coarse_boundary="channel",
base_block=rr.BASE_BLOCK, fine_block=rr.FINE_BLOCK, fine_objects=(body,),
observe_raw_exchange=True, observe_window_exchange=True))
from CelerisLab.lbm.channel import channel_masks
from CelerisLab.lbm.refinement import ACTIVE
from CelerisLab.lbm.descriptors import SOLID
masks = [channel_masks(pair.coarse_shape)[0] & ~pair.covered,
(pair.fine_kind == ACTIVE)
& ((host.flags.reshape(pair.fine_shape) & SOLID) == 0)]
backend.initialize(rr.initial_state(pair.coarse_shape, (0.0, 0.0), 1.0, root=True),
rr.initial_state(pair.fine_shape, pair.fine_origin, 0.5))
probe_p = dict(p, center=[(80.5 - pair.fine_origin[0]) / 0.5 - 0.5,
(81.0 - pair.fine_origin[1]) / 0.5 - 0.5], radius=40.0)
else:
tmp = Path(stack.enter_context(TemporaryDirectory()))
(tmp / "lbm.json").write_text(json.dumps(cfgdict))
(tmp / "body.json").write_text(json.dumps(bodydict))
sim = stack.enter_context(Simulation(str(tmp / "lbm.json"), str(tmp / "body.json"),
device_id=0))
sim.initialize()
probe_p = p
fluid = (sim.field.flag.reshape(p["ny"], p["nx"]) & FLUID) != 0
begin = 0
while begin < lp["steps"]:
rr.check_deadline(a.deadline)
n = min(lp["interval"], lp["steps"] - begin)
if refined:
impulse = rr.advance_refined_interval(backend, n, a.deadline, "window")
fields = [rr.macros(g) for g in backend.download()]
rho, ux, uy = fields[1]
fluid = masks[1]
vals = [tuple(v[m] for v in f) for m, f in zip(masks, fields)]
else:
impulse, done = np.zeros(2), 0
while done < n:
batch = min(100, n - done)
sim.run(batch)
impulse += sim.read_force(0).astype(np.float64) * batch
done += batch
m = sim.get_macroscopic()
rho, ux, uy = [np.asarray(m[k], np.float64).reshape(p["ny"], p["nx"])
for k in ("rho", "ux", "uy")]
vals = [(rho[fluid], ux[fluid], uy[fluid])]
begin += n
row = dict(step=begin, tstar=begin * rr.SPEED / p["diameter"],
**sample(impulse, n, p["diameter"],
h.pressure_probes(rho, fluid, probe_p)["dp"]),
rho_min=float(min(v[0].min() for v in vals)),
rho_max=float(max(v[0].max() for v in vals)),
max_mach=float(max(np.sqrt(3 * (v[1]**2 + v[2]**2)).max() for v in vals)))
rr.ensure_finite(row)
rows.append(row)
if not healthy(row):
break
summary = summarize(rows) if healthy(rows[-1]) else dict(status="UNHEALTHY", steady=False,
verdict=None)
return dict(case=case, collision=a.collision, lattice=lp, rows=rows, **summary)
def plan(collision="SRT"):
return dict(re=RE, collision=collision, tstar_max=TSTAR_MAX, sample_tstar=SAMPLE_TSTAR,
window_tstar=WINDOW_TSTAR, bands=BANDS, range_limits=STEADY_RANGE, slope_limits=STEADY_SLOPE,
deviations=DEVIATIONS, pressure_scale=U_PHYS**2,
refined_root=lattice_parameters(40), refined_fine_tau=0.5 + 3 * 2 * rr.SPEED * 40 / RE,
uniform=lattice_parameters(80),
label="compared against the official reference bands (non-canonical neq_extrap outlet, zou_he_local inlet); not a full benchmark certification")
def main():
parser = argparse.ArgumentParser(description=__doc__.splitlines()[0])
parser.add_argument("--case", choices=["refined", "uniform", "both"], default="refined")
parser.add_argument("--collision", choices=["SRT", "MRT"], default="SRT")
parser.add_argument("--source", type=Path, default=rr.DEFAULT_SOURCE)
parser.add_argument("--output", type=Path, required=True)
parser.add_argument("--plan", action="store_true", help="Write the frozen plan; no CUDA")
parser.add_argument("--max-wall-seconds", type=float)
a = parser.parse_args()
a.source = a.source.resolve()
a.output.mkdir(parents=True, exist_ok=False)
(a.output / "plan.json").write_text(json.dumps(plan(a.collision), indent=2, allow_nan=False))
if a.plan:
return
if not a.max_wall_seconds or a.max_wall_seconds <= 0 or not os.environ.get("CUDA_VISIBLE_DEVICES"):
raise SystemExit("GPU run needs --max-wall-seconds > 0 and explicit CUDA_VISIBLE_DEVICES")
h, _ = rr.helpers(a.source)
rr.config = config # host_geometry builds its root configuration through this name
a.deadline = time.monotonic() + a.max_wall_seconds
cases = ["refined", "uniform"] if a.case == "both" else [a.case]
results = [run_case(a, h, case) for case in cases]
(a.output / "result.json").write_text(json.dumps(results, indent=2, allow_nan=False))
if __name__ == "__main__":
main()
+19 -1
View File
@@ -74,7 +74,25 @@ def cv(g, fluid, origin, rectangle, nu, h=0.5):
Cauchy stress from centred velocity gradients, NOT postcollision non-equilibrium.
Rectangle faces lie on cell edges; fluid mask excludes the staircase cylinder.
"""
rho, mom, vel = moments(g)
return _cv_quantities(*moments(g), fluid, origin, rectangle, nu, h)
def cv_from_macros(rho, ux, uy, fluid, origin, rectangle, nu, h=0.5):
"""Same CV calculation from public macros, in one common length/time frame.
``origin`` is the lower cell edge, ``h`` the cell width, and ``nu`` uses
that frame. Returns [mass, Px, Py] inventory and outward total flux.
Crop fields/mask together and translate origin before calling if desired.
No boundary-exchange observation enters this independent estimator.
"""
rho = np.asarray(rho, np.float64)
if rho.ndim != 2 or any(np.shape(v) != rho.shape for v in (ux, uy, fluid)):
raise ValueError("CV macros and fluid mask must have matching 2D shapes")
vel = np.asarray([ux, uy], np.float64)
return _cv_quantities(rho, rho[None] * vel, vel, fluid, origin, rectangle, nu, h)
def _cv_quantities(rho, mom, vel, fluid, origin, rectangle, nu, h):
x0, y0, x1, y1 = np.rint((np.array(rectangle) - np.tile(origin, 2)) / h).astype(int)
np.testing.assert_allclose(
np.array([x0, y0, x1, y1]) * h + np.tile(origin, 2), rectangle, atol=1e-12
+276 -38
View File
@@ -17,8 +17,109 @@ HERE = Path(__file__).resolve().parent
DEFAULT_SOURCE = HERE.parents[1]
BOUNDS = (40, 24, 320, 140)
BASE_BLOCK = (2, 881) # Exact 166 x 881 domain; no geometric padding.
FINE_BLOCK = (8, 8) # 240 x 568 including four fine halo cells.
FINE_BLOCK = (8, 8) # Wide 240 x 568 or compact 168 x 168, including fine halos.
SPEED = 0.01
JET_PEAK = 0.001
JET_WINDOWS = [(t, t + 10) for t in range(250, 300, 10)]
CV_CONTOURS = np.array([(48., 44., 160., 120.), (44., 36., 180., 128.)])
PLACEMENTS = {"wide": BOUNDS, "compact": (48, 48, 128, 128)}
COMPACT_CV_CONTOURS = np.array([(52., 52., 112., 112.), (50., 50., 120., 120.)])
def selected_cases(selection="both", uniform_diameter=80):
return [(case, diameter) for case, diameter in (("uniform", uniform_diameter), ("refined", 40))
if selection in ("both", case)]
def uniform_origin(diameter):
h = 40 / diameter
return (.5 - .5*h, 1 - h)
def cv_contours(refined, diameter, placement="wide"):
contours = CV_CONTOURS if placement == "wide" else COMPACT_CV_CONTOURS
return contours if refined else contours + [20/diameter, 0., 20/diameter, 0.]
def cv_selected(step, diameter, mode):
return mode == "pilot" or round(290 * diameter / SPEED) <= step <= round(300 * diameter / SPEED)
def cv_snapshot(rho, ux, uy, fluid, origin, refined, begin, n, diameter, impulse, placement="wide"):
"""Cropped public macros only; all inventories, fluxes and impulses use root units."""
from run_jet_circle_cv import cv_from_macros
rectangles = cv_contours(refined, diameter, placement)
h_cell = .5 if refined else 40 / diameter
origin = np.asarray(origin, dtype=float)
x0, y0, x1, y1 = np.rint((rectangles[-1] - np.tile(origin, 2)) / h_cell).astype(int)
selection = np.s_[y0-2:y1+2, x0-2:x1+2]
cropped_origin = origin + h_cell * np.array([x0-2, y0-2])
fields = [v[selection] for v in (rho, ux, uy, fluid)]
values = [cv_from_macros(*fields, cropped_origin, rect, .004, h=h_cell)
for rect in rectangles]
h_native = 1.0 if refined else 40 / diameter
return dict(step=begin+n, tstar=(begin+n)*SPEED/diameter,
time_root=(begin+n)*h_native, interval_start_root=begin*h_native,
interval_dt_root=n*h_native,
interval_impulse_root=(np.asarray(impulse)*h_native**2).tolist(),
inventory=[inventory.tolist() for inventory, _ in values],
outward_flux=[flux.tolist() for _, flux in values])
def public_jets(center, radius, scenario):
"""Same physical apertures; caller supplies its public geometry frame."""
if scenario == "none":
return ()
from CelerisLab.body.jets import Jet, Sector, Radial
peak = 0.0 if scenario == "zero" else JET_PEAK
return tuple(
Jet(Sector(center, angle, math.pi / 12, radius * 1.005),
Radial(center, inward=False), "parabolic", amplitude)
for angle, amplitude in ((math.pi / 2, peak), (3 * math.pi / 2, -peak))
)
def jet_interval(handle, scenario, begin, n, diameter):
"""Apply a reversal only at a completed interval boundary, before advancing."""
if scenario != "none":
boundaries = [round(t * diameter / SPEED) for t in (250, 260, 270, 280, 290, 300, 305)]
n = min([n] + [step - begin for step in boundaries if step > begin])
if scenario != "reverse":
return n, None
switch = round(300 * diameter / SPEED)
if begin < switch:
return min(n, switch - begin), None
if begin == switch:
handle.set_jet_amplitude(0, -JET_PEAK)
handle.set_jet_amplitude(1, JET_PEAK)
return n, dict(step=begin, tstar=300.0, amplitudes=[-JET_PEAK, JET_PEAK])
return n, None
def jet_diagnostics(rows, scenario):
"""Raw interval-weighted diagnostics only; no driven-flow qualification gate."""
windows = JET_WINDOWS + ([(300, 305)] if scenario == "reverse" else [])
result = []
for start, end in windows:
selected = [r for r in rows if start <= r["tstar_force"] < end]
if not selected:
continue
if any(2 * r["tstar_force"] - r["tstar"] < start - 1e-9
or r["tstar"] > end + 1e-9 for r in selected):
raise ValueError("Jet diagnostic interval crosses a window boundary")
weights = np.array([2 * (r["tstar"] - r["tstar_force"]) for r in selected])
record = dict(start_tstar=start, end_tstar=end, samples=len(selected),
covered_tstar=float(weights.sum()),
complete=bool(np.isclose(weights.sum(), end - start, rtol=0, atol=1e-9)))
for key in ("cd", "cl"):
values = np.array([r[key] for r in selected])
record[key] = dict(mean=float(np.average(values, weights=weights)),
min=float(values.min()), max=float(values.max()),
rms=float(np.sqrt(np.average(values**2, weights=weights))))
result.append(record)
return result
def helpers(source):
@@ -39,26 +140,34 @@ def helpers(source):
return h, periodic
def config(h, diameter, collision="SRT"):
def config(h, diameter, collision="SRT", jet_scenario="none"):
cfg, body, p = h.make_config(diameter, SPEED, collision, "neq_extrap", "zou_he_local")
cfg["method"]["outlet"]["srt_neq_damp"] = 0.5
if jet_scenario != "none":
if collision != "MRT":
raise ValueError("Public Jet scenarios require MRT")
cfg["method"]["ddf_shifting"] = False
return cfg, body, p
def plan(h, collision="SRT", observation_mode="last_base_step"):
_, _, c = config(h, 40, collision)
_, _, f = config(h, 80, collision)
x0, y0, x1, y1 = BOUNDS
def plan(h, collision="SRT", observation_mode="last_base_step", jet_scenario="none", uniform_diameter=80, placement="wide"):
_, _, c = config(h, 40, collision, jet_scenario)
_, _, f = config(h, uniform_diameter, collision, jet_scenario)
bounds = PLACEMENTS[placement]
x0, y0, x1, y1 = bounds
fine_active = 4 * (x1 - x0) * (y1 - y0)
coarse_uncovered = c["nx"] * c["ny"] - fine_active // 4
return dict(
status="prepared_not_run",
collision=collision,
jet_scenario=jet_scenario,
ddf_shifting=jet_scenario == "none",
observation_mode=observation_mode,
root_gpu_gates_required=True,
root=c,
uniform=f,
bounds_root_edge=list(BOUNDS),
bounds_root_edge=list(bounds),
fine_origin_root_edge=[x0 - 2, y0 - 2],
physical_patch_m=[
(x0 - 0.5) * c["dx"],
(y0 - 1) * c["dx"],
@@ -78,19 +187,31 @@ def plan(h, collision="SRT", observation_mode="last_base_step"):
physical_viscosity_m2_s=0.001,
finest_dx_m=f["dx"],
finest_dt_s=f["dt"],
refined_finest_dx_m=c["dx"]/2,
refined_finest_dt_s=c["dt"]/2,
approximate_leaf_cell_ratio=(coarse_uncovered + fine_active)
/ (f["nx"] * f["ny"]),
approximate_collision_work_ratio=(coarse_uncovered + 2 * fine_active)
/ (2 * f["nx"] * f["ny"]),
/ ((uniform_diameter/40) * f["nx"] * f["ny"]),
cost_caveat="Geometry-only estimates include ghosts/solids; exclude block halos, transfers, observation and launch overhead. Not measured speedup.",
sampling_offset="For origin (38,22), fine physical x=(j+75.5)*dx80 versus uniform i*dx80: half-fine-cell x offset. Fine physical y=(k+42.5)*dx80 equals uniform (l-.5)*dx80 at l=k+43: y samples align. Body, wall and source planes coincide.",
sampling_offset="Uniform nodes map to root edges X=.5+i*(40/D), Y=1+(j-.5)*(40/D). Refined centers are fine_origin_root_edge+(index+.5)*.5. Body, wall and source planes coincide; compare observables, not pointwise arrays.",
outlet=(
"SRT pressure NEQ, all nine fneq damped by .5, no backflow clamp; noncanonical DFG outlet"
if collision == "SRT" else
"MRT pressure NEQ, unknowns q2/6/8 extrapolated; no backflow clamp; noncanonical DFG outlet"
),
modes={"pilot_tstar": 5.0, "full_tstar": 300.0},
modes={"pilot_tstar": 5.0, "full_tstar": 305.0 if jet_scenario == "reverse" else 300.0},
observation_dense_tstar=0.02,
**(dict(jets=dict(
uniform_origin_node=f["center"], refined_origin_root_edge=[80.5, 81.0],
angles_rad=[math.pi / 2, 3 * math.pi / 2], half_width_rad=math.pi / 12,
radial_extent_over_radius=[0.0, 1.005],
field="Radial(outward)", profile="parabolic", condition="velocity",
initial_amplitudes=[0.0, 0.0] if jet_scenario == "zero" else [JET_PEAK, -JET_PEAK],
reversal_tstar=300.0 if jet_scenario == "reverse" else None,
diagnostic_windows_tstar=JET_WINDOWS + ([(300, 305)] if jet_scenario == "reverse" else []),
transfer="constant", driven_qualification="not assessed",
)) if jet_scenario != "none" else {}),
)
@@ -126,7 +247,7 @@ def initial_state(shape, origin, spacing, height=164.0, speed=SPEED, root=False)
return w * (1 + 3 * cu + 4.5 * cu * cu - 1.5 * velocity * velocity)
def host_geometry(source, h, collision="SRT"):
def host_geometry(source, h, collision="SRT", jet_scenario="none", placement="wide"):
"""Production donor/transfer and complete cut-link checks, without CUDA."""
from CelerisLab.config import load_lbm_config
from CelerisLab.lbm.refinement import FixedPatch2D, prepare_fine_boundary
@@ -139,12 +260,12 @@ def host_geometry(source, h, collision="SRT"):
from CelerisLab.body.geometry.circle import CircleGeometry
from CelerisLab.body.objects import SimObject
cfgdict, _, _ = config(h, 40, collision)
cfgdict, _, _ = config(h, 40, collision, jet_scenario)
with TemporaryDirectory() as tmp:
p = Path(tmp) / "cfg.json"
p.write_text(json.dumps(cfgdict))
cfg = load_lbm_config(str(p))
pair = FixedPatch2D.from_config(cfg, BOUNDS)
pair = FixedPatch2D.from_config(cfg, PLACEMENTS[placement])
layout = BlockLayout2D.build(cfg.ny, cfg.nx, *BASE_BLOCK)
validate_channel_config(cfg, [BASE_BLOCK, FINE_BLOCK])
targets = blocked_base_tables(pair, layout, np.argsort(pair.coalesce_coarse))[1]
@@ -153,18 +274,41 @@ def host_geometry(source, h, collision="SRT"):
body = SimObject(
0, geometry=CircleGeometry(80.5, 81.0, 20.0), center=(80.5, 81.0), radius=20.0
)
host = prepare_fine_boundary(cfg, pair, (body,), _shifted_blocked=True)
host = prepare_fine_boundary(
cfg, pair, (body,), jets=public_jets((80.5, 81.0), 20.0, jet_scenario),
_shifted_blocked=jet_scenario == "none",
)
return cfg, pair, body, host
def verify_source(source, collision="SRT", observation_mode="last_base_step"):
def verify_source(source, collision="SRT", observation_mode="last_base_step", jet_scenario="none", observe_cv=False):
if collision not in ("SRT", "MRT"):
raise ValueError("Matched collision must be SRT or MRT")
if observation_mode not in ("last_base_step", "window"):
raise ValueError("Unknown refined observation mode")
if observe_cv and jet_scenario == "none":
raise ValueError("--observe-cv requires an explicit public Jet scenario")
name = ("source_manifest_window.json" if observation_mode == "window" else
"source_manifest.json" if collision == "SRT" else "source_manifest_mrt.json")
expected = json.loads((HERE / "data/refined_dfg" / name).read_text())
if jet_scenario != "none":
if collision != "MRT" or observation_mode != "window":
raise ValueError("Public Jet scenarios require MRT and --exchange-window")
import subprocess
sys.path.insert(0, str(HERE))
from source_provenance import checkout_provenance
paths = set(expected["sha256"])
if observe_cv:
paths.add("tests/validation/run_jet_circle_cv.py")
paths.update(subprocess.check_output(
["git", "-C", str(source), "ls-files", "src"], text=True).splitlines())
return dict(
source_capture="current checkout, not historical DFG qualification",
**checkout_provenance(source), observation_mode=observation_mode,
sha256={name: hashlib.sha256((source / name).read_bytes()).hexdigest()
for name in sorted(paths)},
)
for name, digest in expected["sha256"].items():
if hashlib.sha256((source / name).read_bytes()).hexdigest() != digest:
raise RuntimeError("Source mismatch: " + name)
@@ -219,29 +363,33 @@ def run_case(a, h, periodic, case):
from contextlib import ExitStack
refined = case == "refined"
cfgdict, bodydict, p = config(h, 40 if refined else 80, a.collision)
cap = 5.0 if a.mode == "pilot" else 300.0
cfgdict, bodydict, p = config(h, 40 if refined else a.uniform_diameter, a.collision, a.jet_scenario)
cap = 5.0 if a.mode == "pilot" else (305.0 if a.jet_scenario == "reverse" else 300.0)
max_steps = math.ceil(cap * p["diameter"] / SPEED)
rows = []
healthy = True
step_seconds = 0.0
cv_seconds, cv_samples = 0.0, 0
amplitude_changes = []
started = time.monotonic()
check_deadline(a.deadline)
dest = a.output / case
dest.mkdir()
with ExitStack() as stack:
cv_out = stack.enter_context((dest / "cv_history.jsonl").open("w")) if a.observe_cv else None
if refined:
cfg, pair, body, host = host_geometry(a.source, h, a.collision)
cfg, pair, body, host = host_geometry(a.source, h, a.collision, a.jet_scenario, a.placement)
context = stack.enter_context(CudaContext(0))
backend = stack.enter_context(
FixedPatchStepper(
cfg,
BOUNDS,
PLACEMENTS[a.placement],
context=context,
coarse_boundary="channel",
base_block=BASE_BLOCK,
fine_block=FINE_BLOCK,
fine_objects=(body,),
jets=public_jets((80.5, 81.0), 20.0, a.jet_scenario),
observe_raw_exchange=True,
**({"observe_window_exchange": True} if a.observation_mode == "window" else {}),
)
@@ -274,6 +422,9 @@ def run_case(a, h, periodic, case):
sim = stack.enter_context(
Simulation(str(tmp / "lbm.json"), str(tmp / "body.json"), device_id=0)
)
for index, jet in enumerate(public_jets(p["center"], p["radius"], a.jet_scenario)):
if sim.add_jet(jet) != index:
raise RuntimeError("Unexpected public Jet registration index")
sim.initialize()
probe_p = p
fluid = (sim.field.flag.reshape(p["ny"], p["nx"]) & FLUID) != 0
@@ -290,6 +441,10 @@ def run_case(a, h, periodic, case):
else 0.5
)
n = min(max(1, round(width * p["diameter"] / SPEED)), max_steps - begin)
n, change = jet_interval(backend if refined else sim, a.jet_scenario,
begin, n, p["diameter"])
if change is not None:
amplitude_changes.append(change)
impulse = np.zeros(2)
tick = time.monotonic()
if refined:
@@ -359,6 +514,19 @@ def run_case(a, h, periodic, case):
/ SPEED,
**h.pressure_probes(rho, fluid, probe_p),
)
if a.jet_scenario != "none":
row.update(step_start=begin, tstar_start=begin * SPEED / p["diameter"],
interval_steps=n, impulse_x=float(impulse[0]),
impulse_y=float(impulse[1]))
if a.observe_cv and cv_selected(begin+n, p["diameter"], a.mode):
tick = time.monotonic()
record = cv_snapshot(rho, ux, uy, fluid,
pair.fine_origin if refined else uniform_origin(p["diameter"]),
refined, begin, n, p["diameter"], impulse, a.placement)
cv_out.write(json.dumps(record, allow_nan=False) + "\n")
cv_out.flush()
cv_samples += 1
cv_seconds += time.monotonic() - tick
check_deadline(a.deadline)
ensure_finite(row)
rows.append(row)
@@ -402,14 +570,24 @@ def run_case(a, h, periodic, case):
steps=begin,
startup_seconds=startup,
step_seconds=step_seconds,
observation_and_overhead_seconds=time.monotonic() - started - startup - step_seconds,
wall_seconds=time.monotonic() - started,
force="raw stationary-body link momentum reaction, per-unit-depth; average over entire observation interval; normalized in each base lattice",
mass_units="rho_reference * m^2 per unit depth",
flux_units="rho_reference * m^2/s per unit depth",
pressure="postcollision end-sample; physical pressure difference / (rho_reference * 1 m/s squared)",
suite_validated=False,
**periodic.assess(rows),
**(periodic.assess(rows) if a.jet_scenario in ("none", "zero") else
dict(periodic=False, checks={}, cycles=[])),
)
if a.jet_scenario != "none":
result.update(jet_diagnostic_windows=jet_diagnostics(rows, a.jet_scenario),
amplitude_changes=amplitude_changes,
pressure_classification=("DFG reference verdict retained, including pressure"
if a.jet_scenario == "zero" else "diagnostic only; no official DFG reference gate"))
if a.observe_cv:
result.update(cv_observation_seconds=cv_seconds, cv_samples=cv_samples,
cv_qualification="not assessed; scalar observations only")
if not healthy:
result["periodic"] = False
reference = json.loads(
@@ -425,7 +603,8 @@ def run_case(a, h, periodic, case):
else (
"pilot_complete"
if a.mode == "pilot"
else ("periodic" if result["periodic"] else "incomplete_periodicity")
else ("driven_diagnostics_complete" if a.jet_scenario in ("fixed", "reverse") else
"periodic" if result["periodic"] else "incomplete_periodicity")
)
)
(dest / "summary.json").write_text(json.dumps(result, indent=2, allow_nan=False))
@@ -464,27 +643,39 @@ def check_deadline(deadline):
)
def verify_pilot(path, manifest, collision="SRT", observation_mode="last_base_step"):
def verify_pilot(path, manifest, collision="SRT", observation_mode="last_base_step", jet_scenario="none", observe_cv=False,
case_selection="both", uniform_diameter=80, placement="wide"):
if path is None:
raise ValueError(
"Full comparison requires --pilot-results from a completed matched pilot"
)
previous = read_finite_json(path / "plan.json")
options = dict(case_selection=(case_selection, "both"), uniform_diameter=(uniform_diameter, 80), placement=(placement, "wide"))
if any(previous.get(k, default) != expected for k, (expected, default) in options.items()):
raise ValueError("Pilot case, resolution or placement differs")
if previous.get("observe_cv", False) != observe_cv:
raise ValueError("Pilot CV observation mode differs")
if previous.get("jet_scenario", "none") != jet_scenario:
raise ValueError("Pilot Jet scenario differs")
if previous.get("observation_mode") != observation_mode:
raise ValueError("Pilot observation mode differs")
if previous.get("collision") != collision:
raise ValueError("Pilot collision differs")
if previous["source_manifest"] != manifest or previous["bounds_root_edge"] != list(
BOUNDS
PLACEMENTS[placement]
):
raise ValueError("Pilot source or frozen geometry differs")
if previous.get("runner_sha256") != runner_hash():
raise ValueError("Pilot runner differs")
calibrated_seconds = 0.0
for case, diameter in (("uniform", 80), ("refined", 40)):
for case, diameter in selected_cases(case_selection, uniform_diameter):
summary = read_finite_json(path / case / "summary.json")
if (
summary.get("observation_mode") != observation_mode
any(summary.get(k, default) != expected for k, (expected, default) in options.items())
or summary.get("observe_cv", False) != observe_cv
or (observe_cv and summary.get("cv_samples") != 250)
or summary.get("jet_scenario", "none") != jet_scenario
or summary.get("observation_mode") != observation_mode
or summary.get("collision") != collision
or summary.get("case") != case
or summary.get("mode") != "pilot"
@@ -537,7 +728,10 @@ def verify_pilot(path, manifest, collision="SRT", observation_mode="last_base_st
raise ValueError("Unhealthy pilot observations")
ready = read_finite_json(path / case / "ready.json")
if (
ready.get("observation_mode") != observation_mode
any(ready.get(k, default) != expected for k, (expected, default) in options.items())
or ready.get("observe_cv", False) != observe_cv
or ready.get("jet_scenario", "none") != jet_scenario
or ready.get("observation_mode") != observation_mode
or ready.get("collision") != collision
or ready.get("case") != case
or ready.get("mode") != "pilot"
@@ -555,9 +749,9 @@ def verify_pilot(path, manifest, collision="SRT", observation_mode="last_base_st
or not 0 < stepping <= wall
):
raise ValueError("Invalid pilot calibration timings")
# Full physical duration is 60 times pilot; dense pilot sampling makes
# Full duration is 60 (or 61 with reversal) times pilot; dense sampling makes
# this conservative for the sparser early full observations. Not a guarantee.
calibrated_seconds += startup + 60 * (wall - startup)
calibrated_seconds += startup + (61 if jet_scenario == "reverse" else 60) * (wall - startup)
return 3 * calibrated_seconds
@@ -566,6 +760,13 @@ def main():
parser.add_argument("--exchange-window", action="store_true",
help="Opt in to refined window-ledger observations on the pinned candidate")
parser.add_argument("--collision", choices=["SRT", "MRT"], default="SRT")
parser.add_argument("--case", choices=["both", "uniform", "refined"], default="both")
parser.add_argument("--uniform-diameter", type=int, choices=[80, 160], default=80)
parser.add_argument("--placement", choices=list(PLACEMENTS), default="wide")
parser.add_argument("--jet-scenario", choices=["none", "zero", "fixed", "reverse"],
default="none", help="Opt in to public unshifted MRT Jets; reverse switches at t*=300 and ends at 305")
parser.add_argument("--observe-cv", action="store_true",
help="Record independent cropped-macro CV samples during pilot or full t*=290..300")
parser.add_argument("--source", type=Path, default=DEFAULT_SOURCE)
parser.add_argument("--output", type=Path, required=True)
parser.add_argument("--mode", choices=["plan", "pilot", "full"], default="plan")
@@ -577,15 +778,26 @@ def main():
help="Required explicit campaign wall-time ceiling for GPU execution",
)
a = parser.parse_args()
if a.uniform_diameter == 160 and a.case != "uniform":
raise ValueError("D160 requires --case uniform; no matched-resolution claim")
if a.placement == "compact" and a.case != "refined":
raise ValueError("Compact placement requires --case refined")
if (a.uniform_diameter != 80 or a.placement != "wide") and a.jet_scenario == "none":
raise ValueError("Resolution/placement variants require an explicit public Jet scenario")
a.source = a.source.resolve()
a.observation_mode = "window" if a.exchange_window else "last_base_step"
manifest = verify_source(a.source, a.collision, a.observation_mode)
manifest = verify_source(a.source, a.collision, a.observation_mode, a.jet_scenario, a.observe_cv)
h, periodic = helpers(a.source)
from source_provenance import checkout_provenance
a.provenance = checkout_provenance(a.source)
a.provenance.update(jet_scenario=a.jet_scenario, ddf_shifting=a.jet_scenario == "none")
a.provenance.update(case_selection=a.case, uniform_diameter=a.uniform_diameter, placement=a.placement)
if a.observe_cv:
a.provenance["observe_cv"] = True
calibration = (
verify_pilot(a.pilot_results, manifest, a.collision, a.observation_mode)
verify_pilot(a.pilot_results, manifest, a.collision, a.observation_mode, a.jet_scenario, a.observe_cv,
a.case, a.uniform_diameter, a.placement)
if a.mode == "full" else None
)
if a.mode != "plan" and (
@@ -602,17 +814,31 @@ def main():
if a.output.exists() and any(a.output.iterdir()):
raise ValueError("Output must be empty/new")
a.output.mkdir(parents=True, exist_ok=True)
specification = plan(h, a.collision, a.observation_mode)
specification = plan(h, a.collision, a.observation_mode, a.jet_scenario, a.uniform_diameter, a.placement)
specification.update(
source_manifest=manifest,
**a.provenance,
gates=periodic.GATES,
reference_gates=periodic.REFERENCE_GATES,
gates=periodic.GATES if a.jet_scenario in ("none", "zero") else None,
reference_gates=periodic.REFERENCE_GATES if a.jet_scenario in ("none", "zero") else None,
runner_sha256=runner_hash(),
wall_time_budget_seconds=budget,
full_pilot_calibration_seconds=calibration,
)
host_geometry(a.source, h, a.collision)
if a.observe_cv:
specification["cv_observation"] = dict(
full_tstar=[290, 300], pilot_tstar=[.02, 5], spacing_tstar=.02,
refined_contours_root=cv_contours(True, 40, a.placement).tolist(),
uniform_contours_root=cv_contours(False, a.uniform_diameter, a.placement).tolist(),
uniform_grid_origin_root=uniform_origin(a.uniform_diameter),
refined_grid_origin_root=specification["fine_origin_root_edge"],
cell_width_root={"uniform": 40/a.uniform_diameter, "refined": .5},
viscosity_root=.004, components=["mass", "Px", "Py"],
units="root lattice per unit depth; outward flux per root time",
interval="Impulse belongs to the interval ending at each snapshot; first retained endpoint (pilot .02, full 290) supplies initial inventory only: exclude its preceding impulse",
qualification="not assessed; trapezoidal integration and time-coarsening are offline",
)
if a.case != "uniform":
host_geometry(a.source, h, a.collision, a.jet_scenario, a.placement)
(a.output / "plan.json").write_text(json.dumps(specification, indent=2))
if a.mode == "plan":
return 0
@@ -621,8 +847,9 @@ def main():
"GPU execution blocked: root GPU gates approval and explicit device selection required"
)
results = []
cases = selected_cases(a.case, a.uniform_diameter)
a.deadline = time.monotonic() + budget
for case in ("uniform", "refined"):
for case, _ in cases:
try:
result = run_case(a, h, periodic, case)
except TimeoutError as exc:
@@ -650,7 +877,12 @@ def main():
status="pilot_only" if a.mode == "pilot" else "incomplete",
matched_case_pass=False,
)
if len(results) == 2 and all(r["healthy"] and r["periodic"] for r in results):
if a.jet_scenario in ("fixed", "reverse"):
comparison.update(status=("pilot_only" if a.mode == "pilot" else "driven_diagnostics_complete")
if len(results) == len(cases) and all(r["healthy"] for r in results) else "invalid_state",
qualification="not assessed; execution completion is not physical acceptance",
jet_diagnostic_windows={r["case"]: r["jet_diagnostic_windows"] for r in results})
if a.case == "both" and len(results) == 2 and all(r["healthy"] and r["periodic"] for r in results):
comparison.update(
status="periodic_comparison",
refined_vs_uniform=periodic.compare(
@@ -660,14 +892,20 @@ def main():
comparison["matched_case_pass"] = comparison["refined_vs_uniform"][
"reference_agreement"
]
if a.case != "both":
comparison.update(status="single_case_" + results[0]["status"],
own_reference_comparison=results[0].get("reference_comparison"))
(a.output / "comparison.json").write_text(
json.dumps(comparison, indent=2, allow_nan=False)
)
return (
0
if len(results) == 2
if len(results) == len(cases)
and all(r["healthy"] for r in results)
and (a.mode == "pilot" or comparison["matched_case_pass"])
and (a.mode == "pilot" or comparison["matched_case_pass"]
or a.jet_scenario in ("fixed", "reverse")
or (a.case != "both" and results[0]["periodic"]
and results[0].get("reference_comparison", {}).get("reference_agreement", False)))
else 2
)