An experimental evaluation of fatigue crack growth S Barter, L Molent, N Goldsmith, R Jones 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 | 123 | 2011 |
Milestone case histories in aircraft structural integrity RJH Wanhill, L Molent, SA Barter, E Amsterdam National Aerospace Laboratory NLR, 2015 | 118 | 2015 |
Recent developments in fatigue crack growth assessment L Molent, R Jones, S Barter, S Pitt International Journal of fatigue 28 (12), 1759-1768, 2006 | 111 | 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 |
Typical fatigue-initiating discontinuities in metallic aircraft structures SA Barter, L Molent, RJH Wanhill International Journal of Fatigue 41, 11-22, 2012 | 95 | 2012 |
Fatigue of beta processed and beta heat-treated titanium alloys R Wanhill, S Barter Springer Science & Business Media, 2011 | 95 | 2011 |
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 |
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy SA Barter, PK Sharp, G Holden, G Clark Fatigue & Fracture of Engineering Materials & Structures 25 (2), 111-125, 2002 | 93 | 2002 |
The effect of laser power density on the fatigue life of laser‐shock‐peened 7050 aluminium alloy Q Liu, CH Yang, K Ding, SA Barter, L Ye Fatigue & fracture of engineering materials & structures 30 (11), 1110-1124, 2007 | 68 | 2007 |
Calculating crack growth from small discontinuities in 7050-T7451 under combat aircraft spectra R Jones, L Molent, SA Barter International Journal of Fatigue 55, 178-182, 2013 | 67 | 2013 |
Fatigue cracking from a corrosion pit in an aircraft bulkhead SA Barter, L Molent Engineering Failure Analysis 39, 155-163, 2014 | 66 | 2014 |
Analysis of cyclic mean stress relaxation and strain ratchetting behaviour of aluminium 7050 W Hu, CH Wang, SA Barter DSTO Aeronautical and Maritime Research Laboratory, 1999 | 64 | 1999 |
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 |
Supersonic particle deposition as a means for enhancing the structural integrity of aircraft structures R Jones, L Molent, S Barter, N Matthews, D Tamboli International Journal of Fatigue 68, 260-268, 2014 | 61 | 2014 |
Evaluation of spectrum fatigue crack growth using variable amplitude data L Molent, M McDonald, S Barter, R Jones International Journal of Fatigue 30 (1), 119-137, 2008 | 60 | 2008 |
The failure of an F/A-18 trailing edge flap hinge S Barter, PK Sharp, G Clark Engineering Failure Analysis 1 (4), 255-266, 1994 | 52 | 1994 |
Crack patching: an experimental evaluation of fatigue crack growth R Jones, S Barter, L Molent, S Pitt Composite structures 67 (2), 229-238, 2005 | 43 | 2005 |
Marker loads for quantitative fractography of fatigue cracks in aerospace alloys SA Barter, L Molent, RJH Wanhill ICAF 2009, Bridging the Gap between Theory and Operational Practice …, 2009 | 39 | 2009 |
Fatigue life recovery in aluminium alloy aircraft structure PK Sharp, Q Liu, SA Barter, P Baburamani, G Clark Fatigue & Fracture of Engineering Materials & Structures 25 (2), 99-110, 2002 | 38 | 2002 |