Documentation
Accepted formats, quantities and rules
Each upload field names the accepted formats and how to export them from the common instrument software; there is no error state, only the list of accepted formats. This page is generated from data/quantities.json, version 2026.09.05-1.
Accepted file formats by measurement
| Quantity | Instrument | Accepted formats | Columns | How to export | Uncertainty after |
|---|---|---|---|---|---|
| grain size d | XRD (Scherrer, Williamson-Hall) | .xy, .xrdml, .raw converted to .xy | two columns, 2theta and intensity | Bruker DIFFRAC.EVA: File, Export, .xy. PANalytical: save .xrdml directly. | 15 % |
| EBSD | .ang, .ctf | TSL .ang or Oxford .ctf grid | AZtec: Export, HKL .ctf. OIM: File, Export, .ang. | 5 % | |
| residual stress sigma_r | XRD sin^2 psi | .xy per psi tilt, psi list | one .xy per tilt plus a text list of psi angles | Export each tilt scan as .xy; list psi values in a .txt. | 10 % |
| wafer curvature (Stoney) | curvature before and after in m^-1 | two numbers | Profilometer or FSM report: read curvature in m^-1. | 10 % | |
| layer thickness h_i | SEM cross-section | image with scale bar | user marks two points | Save .tif with the scale bar burnt in. | 5 % |
| XRR | .xy | 2theta and intensity | Export reflectivity scan as .xy. | 1 % | |
| composition composition | EDS, XPS | .csv, .txt exported tables, .vms | element and atomic fraction | EDS: export quant table as .csv. XPS: save survey as VAMAS .vms. | 8 % |
| linear CTE alpha | dilatometry | .csv T vs dL/L | T in K or C, dL/L | Export the run as .csv with temperature and strain columns. | 3 % |
| Young's modulus E | nanoindentation | .csv load-displacement, vendor summary | load, displacement | Export the indent curves or the summary table as .csv. | 8 % |
| interface toughness G_c | four-point bend, DCB, scratch | .csv load-displacement | load, displacement | Export the test-frame record as .csv. | 20 % |
| activation energy Q | permeation or diffusion couple | .csv t and J | time in s, flux in mol m^-2 s^-1 | ISO 17081 cell: export transient as .csv. | 10 % |
Input quantities
| Symbol | Name | SI unit | Shown as |
|---|---|---|---|
| E | Young's modulus per material, per form, per T | Pa | GPa |
| nu | Poisson ratio | 1 | 1 |
| alpha | linear CTE secant value over the T window; rule R02 handles T dependence | K^-1 | 1e-6 K^-1 |
| sigma_y | yield strength per form and T | Pa | MPa |
| K_Ic | fracture toughness | Pa m^0.5 | MPa m^0.5 |
| G_c | interface toughness with mode mixity psi at which it was measured | J m^-2 | J m^-2 |
| psi | mode mixity phase angle at which G_c was measured | rad | deg |
| h_i | layer thickness | m | um or nm |
| d | grain size from XRD Scherrer or EBSD; rule R10 | m | nm |
| sigma_r | residual stress from XRD sin^2 psi or Stoney; rule R11 | Pa | MPa |
| D0 | Arrhenius prefactor lattice or GB | m^2 s^-1 | m^2 s^-1 |
| Q | activation energy lattice or GB | J mol^-1 | kJ mol^-1 |
| delta | grain-boundary width default 0.5 nm unless source gives | m | nm |
| T | temperature from duty cycle | K | K |
| t | time from duty cycle | s | s |
| p | pressure from duty cycle | Pa | MPa |
| n | number of interlayer steps | 1 | 1 |
| K_bulk_modulus | Bulk modulus isothermal unless the row says otherwise | Pa | GPa |
| alpha_linear | Linear thermal expansion coefficient distinct from alpha: this is the campaign's explicit linear coefficient | 1/K | 1e-6 / K |
| alpha_volumetric | Volumetric thermal expansion coefficient three times the linear coefficient only for an isotropic aggregate | 1/K | 1e-6 / K |
| bond_strength_tensile | Tensile bond strength coating pull-off; not an interface toughness | Pa | MPa |
| c11 | Elastic stiffness c11 single-crystal stiffness tensor component | Pa | GPa |
| c12 | Elastic stiffness c12 single-crystal stiffness tensor component | Pa | GPa |
| c44 | Elastic stiffness c44 single-crystal shear stiffness component | Pa | GPa |
| dK_dP | Pressure derivative of the bulk modulus from an equation-of-state fit | dimensionless | dimensionless |
| density | Density per material, per form | kg/m3 | kg/m3 |
| electrical_resistivity | Electrical resistivity per material, per T | ohm*m | microohm*m |
| flexural_strength | Flexural strength bend test; the row's method states the point count | Pa | MPa |
| hardness | Hardness indentation hardness; the row's method states the scale | Pa | GPa |
| hardness_HV30 | Vickers hardness, HV30 30 kgf load; kept separate from hardness because the load matters | Pa | GPa |
| thermal_conductivity | Thermal conductivity per material, per form, per T | W/(m*K) | W/(m*K) |
| sigma_f | flexural strength as printed by the source, with test_geometry mandatory: three-point and four-point bend on one material differ by a margin that matters, so a strength without its geometry is not a usable number | Pa | MPa |
| sigma_comp | compression strength Consumed by no rule. NEVER substituted for sigma_f, never a fallback for it, and never satisfies a rule asking for it: compression and flexure are different failure modes with different flaw populations, and for these ceramics the compression value is several times the flexural one, so a rule reaching across would answer confidently in the false-pass direction. Registered 8 September 2026 to carry the Smithells Table 27.1 compression column, which had never been loaded. It is deliberately not registered under the symbol for the allowable stress, which is computed by R06 and never stored. Symbol to be confirmed. | Pa | MPa |
| weibull_m | Weibull modulus the number that turns a laboratory strength into a design allowable; without it R06 can only report the margin against mean strength | 1 | 1 |
| specimen_volume_m3 | effective volume under stress the volume the printed strength was measured on, where the source states it; Weibull scaling needs it and the case volume | m^3 | mm^3 |
| G_shear | shear modulus per material, per form, per T Named G_shear rather than G because R16 already derives an energy release rate called G, and two quantities sharing a symbol in one registry is how a unit audit stops being able to check anything. Both are conventionally G in the literature; only one of them can be G here. | Pa | GPa |
| UTS | ultimate tensile strength per material, per form, per T. NOT a yield stress: R16 and the plasticity cap must never reach for it, because a rule taking UTS where no proof stress exists raises the cap threefold on a solder and answers confidently in the false-pass direction. | Pa | GPa |
Rules R00 to R24
- R00 preferred value selection derivedThe derivation is not published on this page.derivation not published on this page
- R01 biaxial modulus derivedThe derivation is not published on this page.derivation not published on this page
- R02 total CTE mismatch derivedThe derivation is not published on this page.derivation not published on this page
- R03 temperature excursion derivedThe derivation is not published on this page.derivation not published on this page
- R04 unrelieved mismatch stress derivedThe derivation is not published on this page.derivation not published on this page
- R05 step stress of a modulus-compensated graded stack derivedThe stress carried across each step of a graded stack, from the total expansion mismatch, the temperature change and the number of steps. The expression that sets it is internal work and is not yet published.derivation not published on this page
- R06 step-stress criterion outputWhether the step stress meets the allowable for the case. The allowable is computed rather than stored, because it depends on the material, the geometry, the stressed volume and a chosen failure probability, and a case may state its own. The criterion is ours and is not yet published.derivation not published on this page
- R07 minimum step count outputThe smallest number of graded steps for which the step-stress criterion is met. It follows from the step stress and the allowable, and is not yet published.derivation not published on this page
- R08 membrane stress in the compliant metal layer derivedThe derivation is not published on this page.derivation not published on this page
- R09 plastic strain derivedThe derivation is not published on this page.derivation not published on this page
- R10 grain size from XRD derivedThe derivation is not published on this page.derivation not published on this page
- R11 residual stress from XRD derivedThe derivation is not published on this page.derivation not published on this page
- R12 effective diffusivity in a polycrystal derivedThe derivation is not published on this page.derivation not published on this page
- R13 barrier breakthrough time outputThe derivation is not published on this page.derivation not published on this page
- R14 pulses to breakthrough outputHow many passes of a duty cycle a barrier survives, by accumulating what each segment consumes of the barrier budget until it is spent. The accumulation model is internal and not yet published.derivation not published on this page
- R15 probability of meeting the barrier criterion outputThe probability that a barrier meets its criterion, by propagating input uncertainty through the model. The choice of input distributions is internal and not yet published.derivation not published on this page
- R16 strain energy release rate derivedG = Z sigma^2 h / E_bar, E_bar = E/(1-nu^2), Z = 0.5 edge delamination, Z = 1.976 channelling crackHutchinson and Suo 1992
- R17 phase angle of loading derivedfrom Dundurs alpha_D, beta_D; edge delamination psi approximately 52 deg for alpha_D = 0Hutchinson and Suo 1992
- R18 fracture margin outputmargin = G_c(psi) / G; G_c(psi) = G_Ic [1 + tan^2((1 - lambda) psi)], lambda default 0.3; delamination if margin < 1Hutchinson and Suo 1992, mixed mode
- R19 weakest interface outputThe derivation is not published on this page.derivation not published on this page
- R20 Sobol indices outputThe derivation is not published on this page.derivation not published on this page
- R21 measure-next ranking outputA ranking of which quantity is worth measuring next, from sensitivity, current relative uncertainty and instrument cost. The heuristic is ours, it has no ground truth outside a scored case, and it is not yet published.derivation not published on this page
- R22 Dundurs parameter derivedThe derivation is not published on this page.derivation not published on this page
- R23 process window outputThe derivation is not published on this page.derivation not published on this page
- R24 membrane gate outputA check that the compliant metal layer can carry the membrane load the ceramic-side layers impose on it. Internal, not yet published.derivation not published on this page
- R25 in-plane expansion on an anisotropic plane outputThe derivation is not published on this page.derivation not published on this page
- R26 polycrystalline moduli from a crystal tensor outputThe derivation is not published on this page.derivation not published on this page
- R27 Poisson ratio derived from a printed pair outputThe derivation is not published on this page.derivation not published on this page
- R28 curvature of a free uniaxial laminate beam outputThe derivation is not published on this page.derivation not published on this page
Data provenance
Every property row carries a source, a quality grade (A measured and peer-reviewed, B handbook, C calculated or estimated, D vendor datasheet), a form and a temperature window. The current seed holds 426 property rows for 100 materials and 59 interface rows, all quality C from the placeholder source, to be replaced by literature values one row at a time.