The elastic-plastic finite element alternating method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures. III: Computational predictions of the NIST multiple site damage experimental results

DOI10.1007/s004660050240zbMath0890.73074OpenAlexW2113119206MaRDI QIDQ1365780

M. García

Publication date: 9 September 1997

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

Full work available at URL: https://doi.org/10.1007/s004660050240

zbMATH Keywords

residual strengthfatigue damage conditions

Mathematics Subject Classification ID

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

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