Average axial stress
σ = P/A
Axial force divided by original cross-sectional area.
Calculate average axial stress, engineering strain, and the elastic modulus implied by the entered load and deformation.
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Average axial stress assumes uniform load distribution. Stress concentrations, nonlinear material response, Poisson effects, necking, buckling, residual stress, and multiaxial stress are not included.
Average normal stress is σ = P/A and engineering strain is ε = ΔL/L. When the response is linear elastic, the ratio σ/ε is Young’s modulus.
Use the Stress & Strain Calculator to estimate average axial normal stress, engineering strain, microstrain, and the implied Young's modulus from axial force, cross-sectional area, deformation, and original length.
Average axial stress is force divided by original cross-sectional area, and engineering strain is change in length divided by original length. In the linear-elastic region, their ratio is Young's modulus.
Uniform uniaxial stress is an idealization. Real parts can have stress concentrations, multiaxial states, plasticity, residual stress, buckling, connection effects, and nonuniform material response.
σ = P/A
Axial force divided by original cross-sectional area.
ε = ΔL/L₀
Change in length divided by original gauge length.
E = σ/ε
For a linear-elastic uniaxial response, stress divided by strain gives Young's modulus.
Use force 50 kN, area 500 mm², deformation 0.5 mm, and original length 1,000 mm.
Result: The numbers are internally consistent with a typical steel-like elastic modulus.
Case: Double axial force with area and deformation relation otherwise held for a purely algebraic check.
Expected: Calculated average stress should double.
Case: Scale force and area by the same factor.
Expected: Calculated stress should remain unchanged.
One microstrain is 10⁻⁶ strain. A strain of 500 µε equals 0.0005.
The stress and engineering strain can still be computed, but σ/ε is no longer Young's modulus once the response is nonlinear or plastic.
No. P/A is the average axial stress. Holes, notches, bending, connections, and local geometry can create much higher local stress.
Shared with the Mechanical Properties and Failure Workbench, which covers plasticity, fatigue, and fracture.
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