Enter load and dimensions to build curves easily. Find modulus, yield, and ultimate strength values. Download tables, share PDFs, and verify every calculation fast.
| Force (N) | Extension (mm) | Comment |
|---|---|---|
| 0 | 0.00 | Start of test. |
| 5000 | 0.05 | Mostly elastic response. |
| 10000 | 0.10 | Still near linear region. |
| 20000 | 0.30 | Plasticity may begin. |
| 28000 | 0.90 | Approaching peak load. |
A stress–strain curve shows how a material behaves under load, from elastic response to failure. This calculator turns raw points into a consistent curve and summarizes modulus, yield, ultimate strength, fracture strain, and energy-related indicators for quick checks.
Engineering stress uses the original area, and engineering strain uses the original gauge length. These definitions are widely used for comparing samples and writing specifications. When you paste force–extension data, the tool calculates σ = F/A and ε = ΔL/L₀.
Early curve slope reflects stiffness. Many steels cluster near 190–210 GPa, aluminum alloys around 65–75 GPa, titanium alloys often 100–120 GPa, and common polymers may fall near 0.5–3 GPa. If your fitted modulus is far outside a plausible range, review units, area, and gauge length.
Modulus estimation depends on the chosen elastic max strain. A practical starting point is 0.002–0.003 for many metals, using at least 5–10 points in that region. If the first points include slack or preload, reduce the range or remove early outliers.
Many materials do not show a sharp yield point. The 0.2% offset method shifts a line parallel to the elastic slope by ε₀ = 0.002, then finds the intersection with your curve. Change the offset to match your lab standard.
Ultimate tensile strength is the maximum stress on the curve. Ductility is often summarized by elongation at break, shown here as the final strain × 100%. Very low elongation can indicate brittle response, while higher values usually suggest more ductile behavior. As reference, mild steels may yield around 200–350 MPa, many structural grades 250–500 MPa, and many aluminum alloys 100–350 MPa, depending on temper and heat treatment. Always compare against the specific datasheet.
The area under the stress–strain curve approximates toughness, or energy absorbed per volume, reported in J/m³. Integrating σ over ε produces J/m³ because 1 Pa equals 1 N/m². This helps compare materials where strength and ductility both matter.
The optional true conversion uses εᵗ = ln(1+ε) and σᵗ = σ(1+ε). It is most meaningful before strong necking, when deformation is more uniform. For post-necking analysis, use measured area reduction methods.
Paste one pair per line using commas or spaces. Choose the correct input mode so the two columns are interpreted properly.
Verify units, gauge length, and area inputs. Adjust the elastic-fit max strain to keep only the linear portion. Noisy first points can distort the slope.
The tool fits an elastic line, shifts it by your offset strain, then interpolates where that line intersects the measured curve.
Toughness is energy absorbed per unit volume until fracture, estimated as the area under the stress–strain curve using trapezoids.
Yes, if you keep a consistent sign convention. Many “tensile” terms may not map directly, so interpret yield and failure with your compression standard.
Jagged curves usually mean sparse sampling, machine noise, or unit mistakes. Add more points, remove obvious outliers, and ensure strain increases down the list.
They are useful during uniform deformation. After necking, true stress needs instantaneous area. Use the option mainly for early-to-mid curve comparisons.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.