Ben Main

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Publications (29)

• Spectrum history effects for small fatigue cracks in aluminium alloy 7050-T7451
  Engineering Fracture Mechanics 2026 DOI: 10.1016/j.engfracmech.2026.112358
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• Unusual Failures Associated with Cracks That Nucleated from Corrosion Damage in Fatigue Tests on AA 7085-T7452 Specimens
  Daren Peng, Andrew Siao Ming Ang, Nam Phan +3 more
  Materials 2026 DOI: 10.3390/ma19153301
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• Influence of in-plane shear on the compression-after-impact (CAI) response of CFRP laminated composites
  Composite Structures 2026 DOI: 10.1016/j.compstruct.2026.120614
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• Navigating Near-Threshold crack growth rate data for aluminium alloy 2024
  International Journal of Fatigue 2026 DOI: 10.1016/j.ijfatigue.2026.109562
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• Fatigue Crack Nucleation and Growth in Recrystallized Annealed Ti‐6Al‐4V Combat Aircraft Structures
  Fatigue & Fracture of Engineering Materials & Structures 2026 DOI: 10.1111/ffe.70198
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• Failure analysis of service fatigue cracks in aircraft structures – Going further
  Engineering Failure Analysis 2026 DOI: 10.1016/j.engfailanal.2025.110207
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• Using marker bands in additively manufactured Ti-6Al-4V to measure small fatigue crack growth rates and equivalent initial damage sizes
  International Journal of Fatigue 2026 DOI: 10.1016/j.ijfatigue.2025.109224
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• A Comparison Between the Growth of Naturally Occurring Three-Dimensional Cracks in Scalmalloy® and Pre-Corroded 7085-T7452 and Its Implications for Additively Manufactured Limited-Life Replacement Parts
  Daren Peng, Shareen S. L. Chan, Ben Main +4 more
  Materials 2025 DOI: 10.3390/ma18245586
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• A fractographic study of fatigue failures in combat aircraft trailing edge flap hinge lug bores in both test and service assets
  Engineering Failure Analysis 2025 DOI: 10.1016/j.engfailanal.2025.109668
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• Navigating Near-Threshold Crack Growth Rate Data for Aluminium Alloy 2024
  Ssrn 2025 DOI: 10.2139/ssrn.5691045
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• Spectrum History Effects for Small Fatigue Cracks in Aluminium Alloy 7050-T7451
  Ssrn 2025 DOI: 10.2139/ssrn.5691044
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• Using Marker Bands in Additively Manufactured Ti-6al-4v to Measure Small Fatigue Crack Growth Rates and Equivalent Initial Damage Sizes
  Ssrn 2025 DOI: 10.2139/ssrn.5209938
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• A fractographic study of fatigue crack growth from a cold expanded fastener hole at an engineering “crack initiation” scale
  Fatigue and Fracture of Engineering Materials and Structures 2024 DOI: 10.1111/ffe.14245
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• Material characterisation of anodising effects on small fatigue crack nucleation in AA7XXX alloys
  Materialia 2024 DOI: 10.1016/j.mtla.2023.101997
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• Equivalent initial damage sizes (EIDS) for type 1C anodised aluminium alloy 7085-T7452 under variable amplitude loading
  Engineering Failure Analysis 2023 DOI: 10.1016/j.engfailanal.2023.107578
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• Material Characterisation of Anodising Effects on Small Fatigue Crack Nucleation in Aa7xxx Alloys
  SSRN 2023 DOI: 10.2139/ssrn.4610047
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• Predicting fatigue crack growth through the small and long crack regimes for a military transport aircraft loading spectrum using FASTRAN
  International Journal of Fatigue 2023 DOI: 10.1016/j.ijfatigue.2023.107576
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• The Australian International Aerospace Congress AIAC 19/20
  Aeronautical Journal 2023 DOI: 10.1017/aer.2023.106
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• On small fatigue crack growth rates in AA7085-T7452
  International Journal of Fatigue 2022 DOI: 10.1016/j.ijfatigue.2021.106704
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• Microstructure and surface finish influences on AA7085-T7452 small fatigue crack growth rates
  Engineering Failure Analysis 2022 DOI: 10.1016/j.engfailanal.2022.106628
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