| An Experimental Evaluation Of Fatigue Crack Growth S Barter, L Molent, N Goldsmith, R Jones Journal Engineering Failure Analysis 12 (1), 99-128, 2005 | 204 | 2005 |
| The lead crack fatigue lifing framework L Molent, SA Barter, RJH Wanhill International Journal of Fatigue 33 (3), 323-331, 2011 | 122 | 2011 |
| Milestone case histories in aircraft structural integrity RJH Wanhill, L Molent, SA Barter, E Amsterdam National Aerospace Laboratory NLR, 2015 | 118 | 2015 |
| Review of fatigue monitoring of agile military aircraft L Molent, B Aktepe Fatigue & fracture of engineering materials & structures 23 (9), 767-785, 2000 | 118 | 2000 |
| Characterisation of equivalent initial flaw sizes in 7050 aluminium alloy L Molent, Q Sun, AJ Green Fatigue & Fracture of Engineering Materials & Structures 29 (11), 916-937, 2006 | 110 | 2006 |
| Interpreting fatigue test results using a probabilistic fracture approach P White, L Molent, S Barter International Journal of Fatigue 27 (7), 752-767, 2005 | 98 | 2005 |
| A comparison of crack growth behaviour in several full-scale airframe fatigue tests L Molent, SA Barter International Journal of Fatigue 29 (6), 1090-1099, 2007 | 95 | 2007 |
| Typical fatigue-initiating discontinuities in metallic aircraft structures SA Barter, L Molent, RJH Wanhill International Journal of Fatigue 41, 11-22, 2012 | 93 | 2012 |
| Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: structural aspects L Molent, RJ Callinan, R Jones Composite structures 11 (1), 57-83, 1989 | 68 | 1989 |
| Fatigue cracking from a corrosion pit in an aircraft bulkhead SA Barter, L Molent Engineering Failure Analysis 39, 155-163, 2014 | 66 | 2014 |
| Observations of crack path changes caused by periodic underloads in AA7050-T7451 P White, SA Barter, L Molent International Journal of Fatigue 30 (7), 1267-1278, 2008 | 62 | 2008 |
| The influence of cyclic stress intensity threshold on fatigue life scatter L Molent, R Jones International Journal of Fatigue 82, 748-756, 2016 | 58 | 2016 |
| A review of equivalent pre‐crack sizes in aluminium alloy 7050‐T7451 L Molent Fatigue & Fracture of Engineering Materials & Structures 37 (10), 1055-1074, 2014 | 51 | 2014 |
| Fatigue crack growth from flaws in combat aircraft L Molent International Journal of Fatigue 32 (4), 639-649, 2010 | 51 | 2010 |
| Managing airframe fatigue from corrosion pits–A proposal L Molent Engineering Fracture Mechanics 137, 12-25, 2015 | 46 | 2015 |
| 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 | 45 | 2019 |
| The equivalence of EPS and EIFS based on the same crack growth life data JP Gallagher, L Molent International Journal of Fatigue 80, 162-170, 2015 | 42 | 2015 |
| Marker loads for quantitative fractography of fatigue cracks in aerospace alloys SA Barter, L Molent, RJH Wanhill Proceedings of the 25th ICAF Symposium of the International Committee on …, 2009 | 39 | 2009 |
| Flight-by-flight fatigue crack growth life assessment W Zhuang, S Barter, L Molent International Journal of Fatigue 29 (9-11), 1647-1657, 2007 | 36 | 2007 |
| The comparison of complex load sequences tested at several stress levels by fractographic examination RA Pell, PJ Mazeika, L Molent Engineering Failure Analysis 12 (4), 586-603, 2005 | 36 | 2005 |
Simon BarterRMIT UniversityVerified email at RMIT.edu.au
