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Stress & Factor of Safety Calculator

Computes internal mechanical stress and verifies structural safety against material yield strength.

Axial Tensile & Compressive Stress Solver

Normal Stress & Factor of Safety

Computes internal mechanical stress σ = F / A and evaluates design safety margins against yield strength σ_y.

Load Preset:
25.00 kN
2.500e-4 m²
36.3 ksi
Material failure threshold
Tensile Bar Stress Distribution & Axial Pull SchematicFFσ = 100 MPaGage Cross Section A = 250 mm²
Calculated Normal Stress
100 MPa
Equivalent to 14,503.8 psi (14.504 ksi)
Factor of Safety (SF = σ_y / σ)
2.5×
Safe Design (SF ≥ 2.0)
Safe Working Capacity
37.43 kN

Max allowable axial load recommended for a standard AISC structural Factor of Safety (SF = 1.67).

Step-by-Step Engineering Proof

Normal Stress σ = F / A = 25,000 N / 250 mm² = 100 MPa (N/mm²)

Factor of Safety SF = σ_yield / σ = 250 MPa / 100 MPa = 2.5

What is Mechanical Stress?

Mechanical stress is the internal force exerted by neighbouring particles of a continuous material across a unit surface area.

Formula & Step-by-Step Calculation

σ = F / A, Factor of Safety (SF) = σ_yield / σ_allowable

Internal axial stress and allowable safety factor.

Worked Step-by-Step Examples

Example 1

A 25 kN tensile force acts on a 250 mm² steel bar (yield strength 250 MPa)

Solution: Stress σ = 100.00 MPa, Factor of Safety SF = 2.50 (Safe)
• σ = 25,000 N / 250 mm² = 100 MPa; SF = 250 / 100 = 2.50

Common Real-World & Academic Use Cases

  • ✓ Structural steel truss member tension/compression checks
  • ✓ Pressure vessel wall hoop stress analysis
  • ✓ Bolted connection shear and tensile load safety

How to Use the Stress & Factor of Safety Calculator

1

Enter Force & Area

Input applied force (N) and cross-sectional area (mm²).

2

Enter Material Yield Strength

Input material yield point (MPa).

3

Inspect Stress & SF

Verify stress level and design safety factor.

Frequently Asked Questions

Q: What is a typical engineering Factor of Safety?

Most civil and mechanical structures use safety factors between 1.5 and 2.5; aerospace applications often use 1.25 to 1.5 to minimize weight.

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