AERO / CANONICAL PUBLIC EVIDENCE INDEX

What has Aero actually demonstrated?

Bounded verification and rejection behavior. Analytical agreement is not experimental validation; a FAIL can be the correct engineering outcome.

Inspect the outcomes—not just the green checks.

6 evidence items

CFD · VERIFICATION + NEGATIVE CONTROLS

MIXED

Verification Bench Rev 1.0

0.053% fine-grid error. Two real failures.

Three pipe grids agree with Poiseuille within 2%. Their errors decrease from 0.996% to 0.243% to 0.053%. The negative controls miss by 13.963% and 99.605%.

Both nozzle treatments fail near-wall readiness. y+ and all-component residual histories distinguish an active-field convergence problem from an ill-conditioned negligible component.

7 new OpenFOAM runs · 295 hashed archive files, including CAD and 5 retained CalculiX decks · 7-page paper. Criteria correction disclosed; not a blinded preregistration.

Scope, reference and retained artifacts

Analytical pipe verification and numerical-readiness rejection, not an experiment or a general nozzle validation. The original Rev 1.0 page, results, and bundle remain frozen.

CFD · ANALYTICAL BENCHMARK

BOUNDED PASS

Channel pressure-budget study

2.5 mm is the smallest tested passing gap.

9 OpenFOAM solves: 3 gaps × 3 grids. At 25 mL/s and a 40 Pa budget, the fine-grid losses are 177.964, 75.078, 38.440 Pa for 1.5, 2.0 and 2.5 mm gaps.

The smaller gaps fail the budget even though numerical checks pass. The 2.5 mm recommendation includes the declared numerical allowance.

200 hashed paper-package artifacts · analytical parallel-plate comparison, profile, residual and conservation checks. Not a sidewall, fitting-loss, or hardware validation.

Conditions, distinct examples and artifacts

This capability study uses 25 mL/s / 40 Pa. The separate interactive default uses 20 mL/s / 70 Pa; their recommendations are not interchangeable.

THERMAL · ANALYTICAL SCREENING

BOUNDED PASS

Cooling-channel layout decision

Layout B: two 2 mm passages.

Three layouts assessed under a 100 W load, 72 °C inner-wall limit and 2 kPa straight-channel pressure budget. Nominal and adverse scenarios are retained.

Energy closure error: 0. The final radial heat-transfer check differs from its analytical reference by 0.001942%.

41 hashed paper-package artifacts. Analytical thermal screening—not thermal CFD or experimental validation. Manifold, contact and boiling effects remain outside the model.

Calculation sources and artifacts

THERMAL + STRUCTURAL · SYNTHETIC PREBENCHMARK

PREBENCHMARK

Samarmad-derived PCHE gate pack

10 runnable gates passed; paper-specific gates remain separate.

A source-derived printed-circuit heat-exchanger packet exercises prediction freezing, criteria hashing, curved-interface pressure and heat-rate transfer, generic OpenFOAM CHT, and generic three-level CalculiX acceptance.

These six operating points are synthetic pipeline tests—not publication results. The later Samarmad-specific run has its own failed numerical outcome and unscored experimental comparison.

STRUCTURAL · NUMERICAL ADEQUACY + REJECTION

MIXED

CalculiX structural extension

21 retained solves. Seven configurations.

Bracket, pressure tubes, a port and thermal restraint were tested at three mesh levels. The port fails mesh sensitivity. The thermal-gradient case passes numerical checks but fails its stress requirement.

Pressure-tube numerical acceptability remains NOT ESTABLISHED with reaction-balance evidence missing. Every configuration retains design readiness NOT ESTABLISHED.

CalculiX 2.20 · Gmsh / CadQuery. Decks and analytical comparisons are bounded evidence, not validated structural design capability.

Per-configuration gates and manifests
ConfigurationNumericalRequirements
bracket
Manifest
PASSPASS
tube
Manifest
NOT_ESTABLISHEDPASS
tube3d
Manifest
NOT_ESTABLISHEDPASS
port
Manifest
FAILNOT_ESTABLISHED
thermal-free
Manifest
PASSPASS
thermal-fixed
Manifest
PASSPASS
thermal-gradient
Manifest
PASSFAIL

All 7 public configuration manifests were checked against their retained files: 0 mismatches. The Verification Bench bundle contains 5 of these retained solve decks, not all 21.

Download retained deck subset ↓

CAD / GEOMETRY · NEGATIVE CONTROL

FAIL — correctly rejected

Imported manifold with a detached sliver

2 solids. Solver not submitted.

The STEP fixture has intersecting ports and fillets. The intact reimport passes topology only; the defective variant violates the single-solid intake contract. No silent deletion or automatic repair.

Two synthetic STEP reimports · OpenCASCADE / CadQuery. This does not establish general imported-CAD robustness.

EXTERNAL BENCHMARKS

Independent measurements. A frozen prediction.

FAIL

Aero Blind Validation Challenge 01

NASA TM-4074 Table XIII: 18 operating points, three grids per point, and 36 experimental targets. Criteria and execution code were publicly committed before production. 54 / 54 attempts finished in the published snapshot.

Reference withheld from solver execution; supervisory setup was not fully blinded. Numerical failures remain visible.

Technical papers / artifacts

The links above lead to the original versioned records. This index does not replace or revise them.

62 committed source artifacts audited. Source snapshot 2ca8e5cbfbdb03515e961be8fc4143f2891e637b. Index hashes establish identity; they do not independently establish scientific validity.

Different evidence answers different questions.

  • Verification / analytical benchmarking: agreement with a known mathematical solution for stated assumptions.
  • Numerical adequacy: mesh, residual, conservation and wall-treatment checks. Necessary, not sufficient for physical accuracy.
  • Negative controls / rejection: deliberately deficient conditions must not be promoted as accepted predictions.
  • External validation: comparison with independent experimental measurements, subject to the declared numerical and modeling limitations.
  • Reproducibility: retained inputs, versions, outputs and hashes permit inspection and reruns—not a guarantee of solver accuracy.

No item here establishes universal Aero validation, certification, autonomous design authority or design readiness.