The elastic-plastic finite element alternating method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures. I: EPFEAM theory. II: Fracture and the \(T^*\)-integral parameter

DOI10.1007/s004660050184zbMath0890.73073OpenAlexW2614154310MaRDI QIDQ1372132

J. Ning

Publication date: 14 July 1998

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s004660050184

zbMATH Keywords

crack growth prediction

Mathematics Subject Classification ID

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

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