Stress • Strain • Young’s Modulus • Poisson’s Ratio
CE StyleInputs
Enter as a ratio (e.g., 0.001 = 0.1%)
Key Results
Details & Derived
Uniaxial: σ = E·ε. Poisson: ν = −εlat/εax.
Plane stress: εx=(σx−νσy)/E, εy=(σy−νσx)/E, γxy=τxy/G, with G=E/[2(1+ν)].
How to use this calculator
Boost GuideQuick start
- Select Units (SI or Imperial).
- Pick a Mode: Uniaxial (solve any of σ, ε, E, ν) or Plane stress (ε from σ, E, ν).
- Enter the requested inputs for the selected Solve for target.
- Click Calculate to see key results and derived moduli.
Core relations: σ = E·ε, ν = −εlat/εax, G = E / [2(1+ν)], K = E / [3(1−2ν)].
Modes
- Uniaxial: Solve one of {σ, ε, E, ν}. Optionally provide ν to also get G and K.
- Plane stress: Provide E, ν, and in-plane stresses σx, σy, τxy to compute εx, εy, γxy and G, K.
Inputs
- Units: SI shows MPa/GPa; Imperial shows ksi/Mpsi.
- Uniaxial (solve σ): Need E and ε.
- Uniaxial (solve ε): Need E and σ.
- Uniaxial (solve E): Need σ and ε (ε ≠ 0).
- Uniaxial (solve ν): Need axial and lateral strains (ν = −εlat/εax).
- Plane stress: Need E, ν, σx, σy, τxy.
- Strain entry: Enter as a ratio (e.g., 0.001 = 0.1%).
Results
- Uniaxial: Solved variable (σ/ε/E/ν), plus optional G, K, and lateral strain if ν is provided.
- Plane stress: εx, εy, γxy, and derived G, K. Inputs are echoed for traceability.
- Strains are shown as ratio and in µε for readability.
Examples
- Steel (uniaxial σ): E = 210 GPa, ε = 0.001 → σ = 210 MPa.
- Find ε: E = 70 GPa, σ = 140 MPa → ε = 0.002 (2000 µε).
- Plane stress: E = 210 GPa, ν = 0.30, σx = 120 MPa, σy = 40 MPa, τxy = 30 MPa → compute εx, εy, γxy and G ≈ 80.8 GPa.
Notes & limits
- Small-strain, linear-elastic assumptions; plasticity, creep, and large strains are not modeled.
- Physically reasonable range: 0 ≤ ν < 0.5 for most isotropic solids.
- Units are consistent per your selection; conversions are handled internally.
- Plane stress assumes σz = 0 (thin plates); use with care for thick bodies.
FAQ & Troubleshooting
Why do I see “–” instead of numbers?
- One or more required inputs are blank or non-numeric. Fill the fields shown for the selected solve mode.
Units look off
- Switch Units first; then enter values (e.g., 200 MPa vs 29 ksi).
Strain entry
- Enter as a ratio: 0.001 = 0.1% = 1000 µε.
Impossible ν?
- Check signs: in tension, lateral strain is typically negative → ν = −εlat/εax.
- Most materials: 0.2–0.4. Values ≥ 0.5 are non-physical for isotropic elastic solids.
γxy seems large/small
- It depends on G = E/[2(1+ν)]; verify E and ν for your material.
Copy-Paste Mini Workflow
1) Choose Units (SI/Imperial) 2) Pick Mode: Uniaxial / Plane stress 3) Choose “Solve for” (if Uniaxial) 4) Fill the requested inputs 5) Press Calculate 6) Read results (σ, ε, E, ν) and derived G, K; plane stress gives εx, εy, γxy
