Public scorecard
What the engine has been checked against
This page separates recorded predictions from outcome-known worked examples and numerical checks. A ledger entry alone does not establish independence, applicability or physical validation. No experimentally validated service domain is established by this page.
ledger at data/predictions.json
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Ledger entries
Logging alone does not establish an independent prediction
0
Recorded scored decisions
0 open; 0 withheld; 0 unrecognised. No accuracy rate asserted.
6
Rules with no external check
and 1 checked on one path only
3
Runs of a published case, worked
read before they were written, so not scored
Worked example, not scored
Niobium diffusion bonded to sapphire, Korn and Cannon 2002
Three specimens from one laboratory, one geometry and one process. Two survived preparation and were tested; the sulphur-doped one broke at the interface during sectioning. The engine is run on each and the observation is printed beside the verdict without any rule reading it. The third has no measured toughness to run against and the engine withholds rather than guesses, which is the coverage number and not the accuracy one. This is not a prediction: the papers were read before the case was written, so it does not enter the log above. Sources: korn2002a, cannon2002b.
| Run | Specimen | Load share | At the interface | G | G_c | Margin | Verdict | Observed |
|---|
| 1 | undoped O21, bonded 1300 C for 1 h | 0.747 | 56 MPa | 25.2 J / m2 | 1 167 J / m2 | 64.7 | pass | survived preparation and was tested to fracture |
| 2 | undoped O11, bonded 1400 C for 3 h | 0.747 | 74 MPa | 44 J / m2 | 115 J / m2 | 3.7 | pass | survived preparation and was tested to fracture |
| 3 | sulphur-doped to 300 atomic ppm, bonded 1300 C for 1 h | 0.747 | 56 MPa | 25.2 J / m2 | not measured | withheld | indeterminate | fractured at the interface during the cutting operation |
Load share between the equal-sharing and thin-layer limits, so neither body carries the mismatch alone.
What the engine says it cannot see
Weakest interface: Niobium / Sapphire, a-plane by fracture, margin 64.74. Observed in the source: survived preparation and was tested to fracture. Meets the static fracture criterion at this interface under cooling from the bonding temperature. Static fracture at this interface is the only mechanism assessed: no time-dependent process, no cyclic loading, no chemical change at the interface and no competing mechanism has been considered, so this is not a statement about the joint. Z 0.5 is read from Hutchinson and Suo Fig. 43, drawn for an elastically homogeneous film on a semi-infinite substrate, and this case meets neither part of that: the pair is not elastically homogeneous, Dundurs alpha 0.53; the substrate is not semi-infinite, film to substrate thickness 1.00. The driving force is therefore computed with a Z outside the range its figure covers, by an amount nobody here has bounded, and the mismatch-dependent solution of their Fig. 53 would settle it. The modulus and Poisson ratio are still plane-unspecified sapphire from Lipkin Table 2 p.4837, reached through the generic path and reported one grade down with the substitution named. The expansion is no longer: this record carries the a-plane index and reaches the corundum crystal, so R25 computes both in-plane coefficients from Merz's axial measurements. The elastic tensor that would replace the modulus is loaded and waiting for the direction-dependent rule. Bending is not modelled. Curvature redistributes stress and can increase its magnitude at some locations; these values are not a general upper bound for a free joint. A constrained joint requires boundary conditions consistent with this membrane model. No free-edge or interfacial traction field is computed. The default mixity law is the tangent form at a lambda of 0.3, supported by Evans 2001's own mode I and mode II pair for a segregated TGO interface, 12.5 and 60 J/m2, whose ratio of 4.80 fixes lambda at 0.302 in the tangent form the engine uses. A justification rather than a check: a ratio between two specimens by two methods is not an external validation, and it agrees with the number already in use, which is the reason to be careful with it rather than the reason to trust it. The toughness was measured at psi -6.5 degrees, close to mode I, and is raised to the edge-delamination angle of 46° by the default tangent law at lambda 0.3. No mixity law is fitted for this interface, so that factor of 1.4 is a convention rather than a measurement. It is the same factor in every run of this case, so it moves the margins together and leaves their order alone. The niobium yield strength used here was measured at room temperature and the case runs at 1573 K. Niobium softens substantially over that interval, so the interlayer is stronger in this calculation than in service and the margin is optimistic. For scale, the niobium alloy WC-103 retains roughly half its room-temperature proof stress at 1500 degrees Celsius (Smithells Table 22.57, pp. 22-157 to 22-158). A niobium yield strength measured at the case temperature would settle it.