| Lessons from a fatigue prediction challenge for an aircraft wing shear tie post B Main, R Evans, K Walker, X Yu, L Molent International journal of fatigue 123, 53-65, 2019 | 46 | 2019 |
| Fatigue crack growth lessons from thirty-five years of the Royal Australian Air Force F/A-18 A/B hornet aircraft structural integrity program B Main, L Molent, R Singh, S Barter International Journal of Fatigue 133, 105426, 2020 | 36 | 2020 |
| The practical need for short fatigue crack growth rate models B Main, M Jones, S Barter International Journal of Fatigue 142, 105980, 2021 | 28 | 2021 |
| On small fatigue crack growth rates in AA7085-T7452 B Main, M Jones, B Dixon, S Barter International Journal of Fatigue 156, 106704, 2022 | 14 | 2022 |
| Enhanced teardown of ex-service F/A-18A/B/C/D centre fuselages L Molent, B Dixon, S Barter, P White, T Mills, K Maxfield, G Swanton, ... ICAF 2009, Bridging the Gap between Theory and Operational Practice …, 2009 | 14 | 2009 |
| Life assessment and repair of fatigue damaged high strength aluminium alloy structure using a peening rework method L Molent, S Barter, B Main Engineering Failure Analysis 15 (1-2), 62-82, 2008 | 10 | 2008 |
| Structural analysis methodology–F/A-18 SB Main | 10* | |
| Predicting fatigue crack growth through the small and long crack regimes for a military transport aircraft loading spectrum using FASTRAN M Jones, B Main, K Maxfield, S Barter, R Das International Journal of Fatigue 171, 107576, 2023 | 7 | 2023 |
| Microstructure and surface finish influences on AA7085-T7452 small fatigue crack growth rates B Main, B Dixon, M Jones, S Barter Engineering Failure Analysis 141, 106628, 2022 | 6 | 2022 |
| Equivalent initial damage sizes (EIDS) for type 1C anodised aluminium alloy 7085-T7452 under variable amplitude loading B Dixon, B Main, S Barter Engineering Failure Analysis 153, 107578, 2023 | 5 | 2023 |
| Outcomes of research into small fatigue crack nucleation and growth in AA7085-T7452 B Main, B Dixon, M Jones, S Barter Proceeding: 31st ICAF Symposium, Delft, Netherlands, 2023 | 3 | 2023 |
| Progress on the pathway to a virtual fatigue test B Dixon, M Burchill, B Main, T Stehlin, R Rigoli ICAF 2019–Structural Integrity in the Age of Additive Manufacturing …, 2020 | 3 | 2020 |
| A fractographic study of fatigue crack growth from a cold expanded fastener hole at an engineering “crack initiation” scale B Main, D Russell, S Barter Fatigue & Fracture of Engineering Materials & Structures, 2024 | 1 | 2024 |
| The Australian Approach to Structural Certification of New Combat Aircraft R Boykett, B Main, M McDonald, M Burchill Aircraft Structural Integrity Program, 2009 | 1 | 2009 |
| Material characterisation of anodising effects on small fatigue crack nucleation in AA7XXX alloys B Main, L Jiang, RKW Marceau, S Barter Materialia 33, 101997, 2024 | | 2024 |
| The Australian International Aerospace Congress AIAC 19/20 A Groszek, B Main, C Bil The Aeronautical Journal 127 (1318), 2067-2067, 2023 | | 2023 |
| Nucleating small fatigue cracks reliably and repeatably M Jones, H Shen, B Main, S Barter, R Das AIAC 2023: 20th Australian International Aerospace Congress: 20th Australian …, 2023 | | 2023 |
| Hawk lead-in-fighter full scale fatigue test-an overview J Turner, B Main, M Attia, R Aaron AIAC 2021: 19th Australian International Aerospace Congress: 19th Australian …, 2021 | | 2021 |
| Acetate replica inspection for aircraft structural integrity management D Russell, B Main, S Barter, J Niclis AIAC 2021: 19th Australian International Aerospace Congress: 19th Australian …, 2021 | | 2021 |
| Evaluation of a PC-9/A Wing Main Spar with Misdrills Using Enhanced Teardown at Resonance B Main, K Muller, M Konak, M Jones, S Sudhakar, S Barter ICAF 2019–Structural Integrity in the Age of Additive Manufacturing …, 2020 | | 2020 |
