Example data table
| Case | Initial length | Final length | Initial diameter | Final diameter | Axial strain | Lateral strain | Poisson’s ratio |
|---|---|---|---|---|---|---|---|
| Steel-like sample | 100.00 mm | 100.20 mm | 10.00 mm | 9.94 mm | 0.002000 | -0.006000 | 0.3000 |
| Polymer-like sample | 50.00 mm | 50.10 mm | 8.00 mm | 7.90 mm | 0.002000 | -0.012500 | 0.6250 (check range) |
Formula used
Poisson’s ratio (ν) relates lateral strain to axial strain under uniaxial loading:
εl = ΔD / D0
ν = − (εl / εa)
For isotropic linear elastic materials, ν can also be computed from elastic constants: ν = E/(2G) − 1 or ν = (3K − E)/(6K).
How to use this calculator
- Select a method: dimensions, strains, or elastic moduli.
- Enter consistent values and keep a clear sign convention.
- Click Calculate to show results above the form.
- Review the range note to detect measurement issues.
- Download CSV or PDF for documentation and reporting.
Microstrain measurement quality
Reliable ν begins with repeatable strain readings. Use axial and lateral gauges with matched gauge factors, and sample at least 100 points in the linear region. For metals, axial strain targets of 500–2500 µε usually stay below yielding while exceeding noise floors. Record temperature, because polymer ν can shift noticeably per 10 °C.
From dimensions to strains
When using length and diameter, compute εa = ΔL/L0 and εl = ΔD/D0 using consistent units. A 100.00 mm specimen that elongates to 100.20 mm has εa = 0.002000. If diameter drops from 10.00 mm to 9.94 mm, εl = −0.006000, giving ν = 0.3000. If your measured D increases under tension, confirm axis labels and gauge polarity.
Interpreting common ranges
Most isotropic engineering solids fall between 0.20 and 0.45. Steels often cluster near 0.27–0.31, aluminum alloys near 0.32–0.35, and many polymers near 0.35–0.49. Values above 0.45 indicate near‑incompressible response and demand careful lateral resolution. Negative ν values can occur in auxetic foams or lattices, but they are uncommon in bulk metals.
Using elastic moduli checks
Cross‑validate ν using E with G or K. With E = 200 GPa and G = 77 GPa, ν = E/(2G) − 1 ≈ 0.2987. If K is available, ν = (3K − E)/(6K) provides an independent route that can reveal fixture slip, end‑constraint effects, or gauge misalignment. Large disagreement between routes is a diagnostic signal.
Derived constants for design
Once ν is known, estimate shear and bulk stiffness: G = E/(2(1+ν)) and K = E/(3(1−2ν)). For E = 70 GPa and ν = 0.33, G ≈ 26.3 GPa and K ≈ 68.6 GPa. These values influence torsion, vibration modes, pressure‑vessel analysis, and acoustic wave speeds.
Reporting and traceability
Document specimen geometry, grip type, loading rate, and sign convention. Report ν with at least four decimals and note the strain window used for regression, such as 0.0005–0.0020. Exporting CSV and PDF outputs supports audits, peer review, and consistent reuse in finite‑element material cards and calculation notes. Include raw ΔL and ΔD values, then archive plots of εl versus εa. A linear fit slope of −ν provides transparency for reviewers and future internal recalibration.