Simon Barter
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An analysis of fatigue crack features at various crack lengths through mating fracture surface pairs
REFERENCES 1. Strength of Materials in the Evolution of Railway Engineering. Dover Publications; 1953: 167-173. 2 Mil-Std-1530d, Department of Defence Standard Practive: Aircraft Structural Integrity Program (Asip), 2016. 3, , . In: ACT Barton, ed. Improving Fatigue Life Predictions with a Crack Growth Rate Material Model Based on Small Crack Growth and Legacy Data. Barton, A.C.T: Engineers Australia, Royal Aeronautical Society; 2017: 56-61. 4, , .
A fractographic study of fatigue crack growth from a cold expanded fastener hole at an engineering “crack initiation” scale
REFERENCES 1. Aging aircraft, the United States Navy experience. In: International Conference on Aircraft Damage Assessment and Repair. 1991. 2, , . Threats to aircraft structural safety, including a compendium of selected structural accidents/incidents. ASC-TR-2010-5002, Aeronautical Systems Centre – Engineering Directorate, United States Air Force, Dayton Ohio, 2010. 3, , . Typical fatigue-initiating discontinuities in metallic aircraft structures. Int J Fatigue. 2012; 41: 11-22. 4, , .
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