Damage tolerance demonstration testing for the Australian F/A-18

DOI10.1016/J.IJFATIGUE.2008.05.009zbMath1419.74225OpenAlexW2002752200MaRDI QIDQ1016276

J. Martínez

Publication date: 5 May 2009

Published in: International Journal of Fatigue (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijfatigue.2008.05.009

zbMATH Keywords

fatigue crack growthlife predictiondamage tolerancefatigue modellingfatigue testingF/A-18 aircraft

Mathematics Subject Classification ID

Fracture and damage (74R99) Theories of fracture and damage (74A45)

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