The graph of stress versus strain in a tensile or compression test; engineering curves use original area A0, while true curves use instantaneous area and reveal continued hardening after necking.

Material testing

Stress–Strain Curve

The graph of stress versus strain in a tensile or compression test; engineering curves use original area A0, while true curves use instantaneous area and reveal continued hardening after necking.

Formula

σeng = F/A0 , εeng = ΔL/L0

Engineering stress and strain relate force F and elongation ΔL to original cross-section A0 and gauge length L0. True stress σtrue = F/A and true strain integrates dL/L for large deformations.

A stress–strain curve is the fundamental record of how a material resists deformation from elastic loading through yielding, strain hardening, necking, and fracture. The engineering curve—force divided by original area—is convenient for specification testing and drops after UTS when necking reduces load despite rising true stress in the neck.

The initial linear elastic segment yields Young’s modulus and proportional limit. Yielding marks the onset of measurable plasticity; proof strengths like Rp0.2 operationalize yield for gradual-yielding materials. The strain-hardening region shows increasing flow stress as dislocation density rises.

Necking begins when the strain-hardening rate can no longer compensate for area loss under constant engineering stress definitions. Toughness (energy to fracture) is the area under the engineering curve up to fracture when plotted in stress–strain space with appropriate units.

Digital acquisition at adequate sampling rate captures serrations (Portevin–Le Chatelier) in some alloys and helps detect instrumentation anomalies such as slip or resonance.

Related standards

Compatible equipment

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