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

QuantityInstrumentAccepted formatsColumnsHow to exportUncertainty after
grain size dXRD (Scherrer, Williamson-Hall).xy, .xrdml, .raw converted to .xytwo columns, 2theta and intensityBruker DIFFRAC.EVA: File, Export, .xy. PANalytical: save .xrdml directly.15 %
EBSD.ang, .ctfTSL .ang or Oxford .ctf gridAZtec: Export, HKL .ctf. OIM: File, Export, .ang.5 %
residual stress sigma_rXRD sin^2 psi.xy per psi tilt, psi listone .xy per tilt plus a text list of psi anglesExport each tilt scan as .xy; list psi values in a .txt.10 %
wafer curvature (Stoney)curvature before and after in m^-1two numbersProfilometer or FSM report: read curvature in m^-1.10 %
layer thickness h_iSEM cross-sectionimage with scale baruser marks two pointsSave .tif with the scale bar burnt in.5 %
XRR.xy2theta and intensityExport reflectivity scan as .xy.1 %
composition compositionEDS, XPS.csv, .txt exported tables, .vmselement and atomic fractionEDS: export quant table as .csv. XPS: save survey as VAMAS .vms.8 %
linear CTE alphadilatometry.csv T vs dL/LT in K or C, dL/LExport the run as .csv with temperature and strain columns.3 %
Young's modulus Enanoindentation.csv load-displacement, vendor summaryload, displacementExport the indent curves or the summary table as .csv.8 %
interface toughness G_cfour-point bend, DCB, scratch.csv load-displacementload, displacementExport the test-frame record as .csv.20 %
activation energy Qpermeation or diffusion couple.csv t and Jtime in s, flux in mol m^-2 s^-1ISO 17081 cell: export transient as .csv.10 %

Input quantities

SymbolNameSI unitShown as
EYoung's modulus
per material, per form, per T
PaGPa
nuPoisson ratio
11
alphalinear CTE
secant value over the T window; rule R02 handles T dependence
K^-11e-6 K^-1
sigma_yyield strength
per form and T
PaMPa
K_Icfracture toughness
Pa m^0.5MPa m^0.5
G_cinterface toughness
with mode mixity psi at which it was measured
J m^-2J m^-2
psimode mixity
phase angle at which G_c was measured
raddeg
h_ilayer thickness
mum or nm
dgrain size
from XRD Scherrer or EBSD; rule R10
mnm
sigma_rresidual stress
from XRD sin^2 psi or Stoney; rule R11
PaMPa
D0Arrhenius prefactor
lattice or GB
m^2 s^-1m^2 s^-1
Qactivation energy
lattice or GB
J mol^-1kJ mol^-1
deltagrain-boundary width
default 0.5 nm unless source gives
mnm
Ttemperature
from duty cycle
KK
ttime
from duty cycle
ss
ppressure
from duty cycle
PaMPa
nnumber of interlayer steps
11
K_bulk_modulusBulk modulus
isothermal unless the row says otherwise
PaGPa
alpha_linearLinear thermal expansion coefficient
distinct from alpha: this is the campaign's explicit linear coefficient
1/K1e-6 / K
alpha_volumetricVolumetric thermal expansion coefficient
three times the linear coefficient only for an isotropic aggregate
1/K1e-6 / K
bond_strength_tensileTensile bond strength
coating pull-off; not an interface toughness
PaMPa
c11Elastic stiffness c11
single-crystal stiffness tensor component
PaGPa
c12Elastic stiffness c12
single-crystal stiffness tensor component
PaGPa
c44Elastic stiffness c44
single-crystal shear stiffness component
PaGPa
dK_dPPressure derivative of the bulk modulus
from an equation-of-state fit
dimensionlessdimensionless
densityDensity
per material, per form
kg/m3kg/m3
electrical_resistivityElectrical resistivity
per material, per T
ohm*mmicroohm*m
flexural_strengthFlexural strength
bend test; the row's method states the point count
PaMPa
hardnessHardness
indentation hardness; the row's method states the scale
PaGPa
hardness_HV30Vickers hardness, HV30
30 kgf load; kept separate from hardness because the load matters
PaGPa
thermal_conductivityThermal conductivity
per material, per form, per T
W/(m*K)W/(m*K)
sigma_fflexural 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
PaMPa
sigma_compcompression 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.
PaMPa
weibull_mWeibull modulus
the number that turns a laboratory strength into a design allowable; without it R06 can only report the margin against mean strength
11
specimen_volume_m3effective 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^3mm^3
G_shearshear 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.
PaGPa
UTSultimate 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.
PaGPa

Rules R00 to R24

  • R00 preferred value selection derived
    The derivation is not published on this page.
    derivation not published on this page
  • R01 biaxial modulus derived
    The derivation is not published on this page.
    derivation not published on this page
  • R02 total CTE mismatch derived
    The derivation is not published on this page.
    derivation not published on this page
  • R03 temperature excursion derived
    The derivation is not published on this page.
    derivation not published on this page
  • R04 unrelieved mismatch stress derived
    The derivation is not published on this page.
    derivation not published on this page
  • R05 step stress of a modulus-compensated graded stack derived
    The 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 output
    Whether 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 output
    The 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 derived
    The derivation is not published on this page.
    derivation not published on this page
  • R09 plastic strain derived
    The derivation is not published on this page.
    derivation not published on this page
  • R10 grain size from XRD derived
    The derivation is not published on this page.
    derivation not published on this page
  • R11 residual stress from XRD derived
    The derivation is not published on this page.
    derivation not published on this page
  • R12 effective diffusivity in a polycrystal derived
    The derivation is not published on this page.
    derivation not published on this page
  • R13 barrier breakthrough time output
    The derivation is not published on this page.
    derivation not published on this page
  • R14 pulses to breakthrough output
    How 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 output
    The 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 derived
    G = Z sigma^2 h / E_bar, E_bar = E/(1-nu^2), Z = 0.5 edge delamination, Z = 1.976 channelling crack
    Hutchinson and Suo 1992
  • R17 phase angle of loading derived
    from Dundurs alpha_D, beta_D; edge delamination psi approximately 52 deg for alpha_D = 0
    Hutchinson and Suo 1992
  • R18 fracture margin output
    margin = G_c(psi) / G; G_c(psi) = G_Ic [1 + tan^2((1 - lambda) psi)], lambda default 0.3; delamination if margin < 1
    Hutchinson and Suo 1992, mixed mode
  • R19 weakest interface output
    The derivation is not published on this page.
    derivation not published on this page
  • R20 Sobol indices output
    The derivation is not published on this page.
    derivation not published on this page
  • R21 measure-next ranking output
    A 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 derived
    The derivation is not published on this page.
    derivation not published on this page
  • R23 process window output
    The derivation is not published on this page.
    derivation not published on this page
  • R24 membrane gate output
    A 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 output
    The derivation is not published on this page.
    derivation not published on this page
  • R26 polycrystalline moduli from a crystal tensor output
    The derivation is not published on this page.
    derivation not published on this page
  • R27 Poisson ratio derived from a printed pair output
    The derivation is not published on this page.
    derivation not published on this page
  • R28 curvature of a free uniaxial laminate beam output
    The 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.