Engineering · Stress, Failure & Materials

Fracture and Material Testing Workbench Calculator

Calculate stress intensity, critical crack size, Paris-law crack growth, elastic energy release, true stress–strain and test-property conversions from entered data.

Engineering · Stress, Failure & Materials

Enter the engineering model

Explicit properties, geometry, units and assumptions
Visual modelSchematic · not to scale
Stress, Failure & Materials: K visual explanationA simplified diagram showing the relationship represented by the selected calculator mode. It is explanatory and not a fabrication, safety or scale drawing.crack tip and stress-intensity relationshipspecimen geometry matters
The diagram explains the selected relationship only. Dimensions, symbols and proportions are illustrative; use the entered values and stated assumptions for the calculation.

Keep every unit basis, sign convention, property source and idealization consistent. Values stay in this browser.

Engineering calculation result

Enter valid values to see the result.

Your entries are calculated in this browser and are not submitted to 365CALCS.COM.

Quick guide

How to use this calculator

  1. Choose the analysis mode that matches the physical model before entering values.
  2. Enter properties, geometry, loads, states and coefficients from one consistent unit and sign convention.
  3. Use the intermediate outputs to audit the relationship, then retain the stated idealization before applying it.

Calculation method

Transparent engineering model

K=Yσ√(πa); Paris growth uses da/dN=C(ΔK)^m; true stress is force/current area and true strain is ln(L/L₀).

The calculator evaluates only the declared relationship and preserves visitor-entered assumptions rather than selecting materials, factors, components or standards.

Worked example

Worked example

For an entered geometry factor Y, stress and crack size, the stress-intensity result exposes every operand rather than hiding a material default.

K=Yσ√(πa); Paris growth uses da/dN=C(ΔK)^m; true stress is force/current area and true strain is ln(L/L₀).

Supported inputs

Precision and limits

Analysis, not approval

Fracture and test results are specimen-, geometry-, environment- and method-dependent. They do not establish fracture safety, inspection acceptance or remaining life.

Standards and properties

Material properties, allowable values, load combinations, safety factors, correlations, manufacturer data, codes and jurisdictional requirements are not supplied automatically.

Units and precision

Use one consistent unit basis. Results retain working precision but cannot be more accurate than the entered measurements and properties.

Privacy

Entered engineering values and results stay in this browser and are not sent to analytics or third parties.