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Stress, Strain, and Structural Failure

Manual: General · Subject: Engineering

Analyze how materials deform under load and how engineers prevent yielding, buckling, fatigue, and fracture.

Internal loading and deformation

Stress and strain

Normal stress is defined as σ=FA\sigma = \frac{F}{A} and normal strain as ε=ΔLL0\varepsilon = \frac{\Delta L}{L_0}. In the linear elastic range, many materials follow Hooke's law: σ=Eε\sigma = E\varepsilon, where EE is Young's modulus.

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Safety factor

Engineers often design with a safety factor to account for uncertainty, variability, and unexpected loading. A safety factor is not a substitute for understanding failure modes.

Common failure modes

Yielding is permanent deformation, buckling is sudden instability under compression, fatigue is failure under repeated loading, and fracture is cracking or separation. Different structures fail in different ways depending on geometry, load history, and environment.

A failure-analysis checklist

  1. 1

    Step 1: Identify the load case and support conditions.

  2. 2

    Step 2: Determine the likely stress concentrations.

  3. 3

    Step 3: Compare operating stress with material limits.

  4. 4

    Step 4: Consider repeated loading, corrosion, and temperature.

  5. 5

    Step 5: Add mitigation such as geometry changes or material upgrades.

Which formula defines normal stress?

What type of failure can happen suddenly in a slender compressed column?

Repeated loading over time most commonly leads to: