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Simon Barter
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An experimental evaluation of fatigue crack growth
S Barter, L Molent, N Goldsmith, R Jones
Engineering failure analysis 12 (1), 99-128, 2005
2022005
The lead crack fatigue lifing framework
L Molent, SA Barter, RJH Wanhill
International Journal of Fatigue 33 (3), 323-331, 2011
1212011
Milestone case histories in aircraft structural integrity
RJH Wanhill, L Molent, SA Barter, E Amsterdam
National Aerospace Laboratory NLR, 2015
1172015
Recent developments in fatigue crack growth assessment
L Molent, R Jones, S Barter, S Pitt
International Journal of fatigue 28 (12), 1759-1768, 2006
1112006
Interpreting fatigue test results using a probabilistic fracture approach
P White, L Molent, S Barter
International Journal of Fatigue 27 (7), 752-767, 2005
972005
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
952007
Fatigue of beta processed and beta heat-treated titanium alloys
R Wanhill, S Barter
Springer Science & Business Media, 2011
932011
Typical fatigue-initiating discontinuities in metallic aircraft structures
SA Barter, L Molent, RJH Wanhill
International Journal of Fatigue 41, 11-22, 2012
922012
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
922002
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
672007
Fatigue cracking from a corrosion pit in an aircraft bulkhead
SA Barter, L Molent
Engineering Failure Analysis 39, 155-163, 2014
662014
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
662013
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
631999
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
612008
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
602008
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
582014
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
521994
Crack patching: an experimental evaluation of fatigue crack growth
R Jones, S Barter, L Molent, S Pitt
Composite structures 67 (2), 229-238, 2005
432005
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
382009
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
372002
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