A combustion-chamber sector coupon, solver-verified and print-ready.
solver run · check these numbers against their artifacts
A curved Inconel 625 combustion-chamber sector test coupon, built to a turbojet OEM's publicly documented envelope. A public-reference demonstrator, ready for bench testing — not engine-validated hardware.
The solver chain it passed
| Stage | Tool | Result |
|---|---|---|
| Mesh integrity | manifold audit | 134,608 triangles, watertight, 0 open edges |
| Manufacturability | LPBF gates | pass — continuous purge path, powder access, overhang |
| Volume mesh | Gmsh | 98,691 nodes / 406,889 tets |
| Structural FEA | CalculiX | axial E = 136.72 GPa · first yield 165.01 MPa |
| Steady conduction | CalculiX | 7.970 W/mK effective · 0.2% vs fast model |
| Pore-scale flow | D3Q19 LBM | k = 410.6 µm² · converged, 1,400 iterations |
Claim discipline: the technical report this coupon
shipped in had its 10 headline numbers machine-compiled against the solver
evidence — verdict ALL_TRACED. This website's numbers get the
same treatment.
What exists today
- Print-ready 3MF/STL files with SHA-256 sums
- Full solver-evidence JSONs for every stage above
- A proposed physical test matrix: dimensional/micro-CT, cold-flow ΔP, thermal coupon, mechanical, thermal cycling
The intended loop: a partner prints the coupon, runs the bench tests, and the measurements feed back into the engine's ground-truth ledger — so the next design generation is calibrated against physical reality, not a textbook.
Back to evidence Bench-test it with us