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Monash engineers improve fatigue life of high-strength aluminum alloys by 25 times

Monash University engineers have demonstrated improvements in the fatigue life of high-strength aluminum alloys by 25 times—a significant outcome for the transport manufacturing industry.

In an open-access paper published in Nature Communications, the researchers reported that the poor fatigue performance of high-strength aluminum alloys was because of weak links called “precipitate free zones” (PFZs).

The team led by Professor Christopher Hutchinson, a Professor of Materials Science and Engineering at Monash University in Australia, was able to make aluminum alloy microstructures that can heal the weak links while in operation (i.e. a form of self-healing).

The improvement in the lifetime of high strength aluminum alloys could be 25 times compared to current state-of-the-art alloys.

Aluminum alloys are the second-most popular engineering alloy in use today. Compared to steel, they are light (1/3 of the density), non-magnetic and have excellent corrosion resistance.

Aluminum alloys are important for transport applications because they are light, which improves fuel efficiency. But, their fatigue properties are notoriously poor compared to steel of similar strength.

Professor Hutchinson said when using aluminum alloys for transport, the design must compensate for the fatigue limitations of aluminum alloys. This means more material is used than manufacturers would like and the structures are heavier than we would like.

Eighty per cent of all engineering alloy failures are due to fatigue. Fatigue is failure due to an alternating stress and is a big deal in the manufacturing and engineering industry. Think of taking a metal paperclip in your hands and trying to break the metal. One cannot. However, if you bend it one way, then the other, and back and forth a number of times, the metal will break.

This is failure by fatigue and it’s an important consideration for all materials used in transport applications, such as trains, cars, trucks and planes.

—Professor Hutchinson

Failure by fatigue occurs in stages. The alternative stress leads to microplasticity (undergoing permanent change due to stress) and the accumulation of damage in the form of a localisation of plasticity at the weak links in the material.

The plastic localization catalyzes a fatigue crack. This crack grows and leads to final fracture.

Using commercially available AA2024, AA6061 and AA7050 aluminum alloys, researchers used the mechanical energy imparted into the materials during the early cycles of fatigue to heal the weak points in the microstructure (the PFZs).


Correlation between fatigue strength and tensile strength for three Al alloys. Zhang et al.

This strongly delayed the localization of plasticity and the initiation of fatigue cracks, and saw enhanced fatigue lives and strengths.

Professor Hutchinson said these findings could be significant for the transport manufacturing industry as the demand for fuel efficient, lightweight and durable aircraft, cars, trucks and trains continues to grow.

Our research has demonstrated a conceptual change in the microstructural design of aluminum alloys for dynamic loading applications. Instead of designing a strong microstructure and hoping it remains stable for as long as possible during fatigue loading, we recognized that the microstructure will be changed by the dynamic loading and, hence, designed a starting microstructure (that may have lower static strength) that will change in such a way that its fatigue performance is significantly improved.

In this respect, the structure is trained and the training schedule is used to heal the PFZs that would otherwise represent the weak points. The approach is general and could be applied to other precipitate hardened alloys containing PFZs for which fatigue performance is an important consideration.

—Professor Hutchinson

This work was funded by the Australian Research Council.


  • Zhang, Q., Zhu, Y., Gao, X. et al. (2020) “Training high-strength aluminum alloys to withstand fatigue. Nat Commun 11, 5198 doi: 10.1038/s41467-020-19071-7



If they can make aluminium parts lighter and safer, all the good.
I wonder when we'll see this in a product ?


This would be good for airplane frames.


If only De Havilland had known this when they designed and made the Comet Mk 1 in 1949-52.

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