What is  Fatigue?

Written by Rahul Verma | Updated: March 29, 2026

What is  Fatigue?

Written by Rahul Verma |  Updated: March 29, 2026

One of the most frequent causes of wear and tear is fatigue. Cyclic stress causes localized, irreversible degradation in metals. Force, vibration, acceleration, deceleration, and thermal expansion/ contraction discrepancies between mating components subjected to repeated heating/cooling cycles are only some of the many potential sources of uniaxial, bending, and torsional stress. When a component or joint sustains localized damage, it is limited to a small area.

The nominal stress operating on a component or joint is often below its yield strength, which can lead to unexpected fatigue. The stress, however, is higher than the nominal stress at a fatigue fracture starting location because of the presence of a stress concentration. More on this to come.

There are 3 conditions

There are three necessary conditions for weariness to set in:

  • Repetitive strain
  • The force exerted must be tensile.
  • When the local stress is high enough, the metal yields.

Steps Involved:

There are three phases to a fatigue fracture:

  • The initial cracking stage. As the material goes through its upper and lower stress cycles, tiny cracks, measuring less than 0.001 mm in length, emerge. Microcracks enlarge and join together through repeated cycling, eventually becoming larger cracks or cracks.
  • Second-stage crack development. The larger breaks propagate further into the substance. Nominal stress on the uncracked part of the metal grows as the cracks expand.
  • Third, once a certain percentage of the cross-section has broken, the remaining intact material is unable to support the weight and cracks due to overload.

Surface fractures

This image depicts the fracture surface of a material that developed a crack due to fatigue. The component’s surface was the initial failure point. After the initial crack formed, it widened with each new force. The crack widened until the uncracked material could no longer bear the weight, and then it fractured in a single stress cycle.

Benchmarks, which may be observed with the naked eye or a low-magnification microscope, are a common feature of the fracture surface. A crack’s beach marks can assist pinpoint its starting point because they develop outward in the same direction as the crack.

A piece of aluminium with a fractured surface, as seen using a scanning electron microscope. The striations manifest themselves as the fatigue crack widens with repeated tension. Each striation formed throughout a stress cycle, revealing the cumulative growth of the crack over time. Fracture striations are not present in all cases of fatigue failure.

Concentrations of Stress

When the nominal stress on a metal is lower than its yield strength, fatigue damage still occurs. Increases in stress due to stress concentrations lead to localized stresses that are greater than the material’s yield strength. Concentrations of stress can be found in places like notches, serial numbers, and blemishes on metal (non-metallic inclusions, voids, laps).

Even if there are no sharp stress concentrations on the surface of the metal, a fatigue crack can nonetheless occur. To create a crack, however, such a metal requires a greater number of cycles than the identical metal with an apparent stress concentration.

Causes of exhaustion in daily life

A component or joint’s fatigue life is often described as the sum of the number of cycles required to develop a crack and the number of cycles required for the crack to grow to failure. When a crack reaches a certain length, it is considered a failure and the part or subassembly is taken out of service. A component or joint failure is another type of failure that frequently occurs without warning.

The fatigue life of a component or joint is affected by a number of design, material, and production parameters, including:

Stress-concentrating mechanical design elements

  • A robust alloy
  • Manufacturing flaws and the presence of nonmetallic impurities.
  • Remaining surface tension
  • The roughness of a surface
  • Resistance to fracture in metals
  • Future articles will go deeper into these contributing elements and methods for enhancing fatigue resistance.

ABOUT AUTHOR

Rahul Verma

Rahul Verma is a dedicated Materials Scientist and Testing Associate with strong expertise in materials characterization, thermal spray coatings, and advanced manufacturing technologies. With a solid foundation in Materials Science & Engineering and hands-on research in additive manufacturing, he specializes in bridging material behavior insights with practical engineering solutions. Currently serving as a Materials Testing Associate at Infinita Lab Inc. (USA), Rahul ensures precise material testing, quality assurance, and customer-focused solutions that help clients overcome complex materials challenges.

His role blends technical rigor with operations and project management, driving efficiency, reliability, and client satisfaction. Rahul’s journey spans academic and industrial research at IIT Patna, where he has contributed to advancements in plasma spray techniques, AI/ML-driven material design, and additive manufacturing.

He has also co-founded GreeNext Materials Group, pioneering sustainable battery regeneration technologies that have a significant impact on both industrial and societal applications. With professional experience in operations leadership, R&D, and client engagement, Rahul brings a results-oriented and analytical approach to materials engineering. He continues to advance innovation in coatings, material performance, and testing methodologies—focusing on durability, sustainability, and real-world applications.

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