Approximate methods for analyzing the growth of large cracks in fatigue damaged aircraft sheet material and lap joints

DOI10.1016/S0168-874X(96)80002-3zbMATH Open0875.73182OpenAlexW1972674470MaRDI QIDQ671733

Xiangyang Deng, J. W. Hutchinson

Publication date: 27 February 1997

Published in: Finite Elements in Analysis and Design (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0168-874x(96)80002-3

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Fracture and damage (74R99)

Related Items (1)

Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skin

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