AERO / SYNTHETIC PREBENCHMARK

PREBENCHMARK · SYNTHETIC ONLY

Printed-circuit heat exchanger, with the answer kept out of the model.

Samarmad-derived geometry and operating conditions were assembled before a prediction bundle was frozen. Missing measurements and properties were completed with marked synthetic estimates so the surrounding CFD → transfer → FEA contracts could be exercised without claiming publication agreement.

10 runnable gates passed · 6 synthetic operating points · paper comparison not established

What this entry means

Runnable pipeline proof: PASS. The frozen packet, criteria, hash verification, curved-interface transfer, generic OpenFOAM CHT run, and generic three-level CalculiX run are retained below.

Physical validation: NOT ESTABLISHED. The paper's measurements were not exposed to the model, and the Samarmad-specific corrugated CFD and PCHE structural cases have not been run.

Model-facing input packet

These are the inputs Aero was allowed to use before the synthetic truth was generated. The source paper is linked for attribution; its results and conclusions are not part of this packet.

Geometry envelope

Configuration
straight baseline and two-way corrugated Model 6
Plate stack
8 plates · 4 mm thick
Channel count
14 per plate · semicircular
Hydraulic diameter
1.5275 mm
Corrugation
0.80 mm amplitude · 12.60 mm wavelength

Operating envelope

Working fluids
water / water
Arrangement
counter-current
Inlet temperatures
293 K cold · 323 K hot
Flow regime
laminar single phase
Reynolds range
300–1900

Synthetic completion: nominal water properties, aluminum solid mechanics, and ±2% channel-diameter / ±1% plate-thickness sensitivity estimates. These are estimates, not transcribed experimental values.

Prediction freeze before synthetic truth

The prediction bundle was sealed and verified before the synthetic pointwise truth existed. The published measurements remain withheld.

RecordState
Prediction frozen before truthTRUE
Publication measurements accessedFALSE
Freeze manifest SHA-256025bf0d8e1056986d3d80662475f723ee824813a9a787904a090a2016f3da4b3
Gate-pack verificationVERIFIED
Criteria SHA-256ca37cf842c210402ff591cbed1737dfaeb93cba9ba0c9739ec796fe9a806e7b9

Gate ledger

The surrounding pipeline contracts are explicit. A passed generic gate is not silently promoted to a Samarmad-specific result.

GateResult
benchmark criteria frozenPASS
curved transfer heat ratePASS
curved transfer pressure integral and forcePASS
generic calculix worker imagePASS
generic openfoam chtPASS
generic openfoam studyPASS
generic three level feaPASS
pche calculix geometryNOT_RUN
pche curved chtNOT_RUN
pche openfoamNOT_RUN
prediction bundle hash and verifyPASS
publication reference validationNOT_ESTABLISHED
publication source eligibilityOPEN
source custody reference separationPASS
source input and synthetic estimate packetPASS
trusted external timestampOPEN

Synthetic operating-point packet

These values are synthetic completions used to exercise the prebenchmark contract. They are not experimental observations.

ReVelocity (m/s)Δp (Pa)Heat duty (W)Effectiveness
3000.197650.2734.60.866
6000.3941300.41295.80.764
9000.5911950.61738.70.683
12000.7892600.92097.00.618
15000.9863251.12392.80.564
19001.2494118.02715.50.506

Open gates and next step

The following items remain open in this revision: pche calculix geometry, pche curved cht, pche openfoam, publication reference validation, publication source eligibility, trusted external timestamp.

To turn this into a scored paper benchmark, Aero still needs a rights-cleared source-custody record, complete pre-result inputs, sealed pointwise measurements and uncertainty, corrugated PCHE CAD, three target-specific OpenFOAM CHT levels, PCHE-specific CalculiX mapping, and an external timestamp before the reference is revealed.

Source custody status: CONDITIONAL_LOCAL_SYNTHETIC_ONLY. The source is linked for attribution only; no full text or adapted publication measurements are redistributed here.