Q1372132
type: Item
instance of: scholarly article
title: 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
zbMATH Open document ID: 0890.73073
author: J. Ning
published in: Computational Mechanics
publication date: 1998-07-14T00:00:00Z
review text: This excellent work presents a summary of the elastic-plastic finite element alternating method, an algorithms for fracture analysis and crack growth prediction. Additionally, the authors provide a complete description of the \(T^*\)-integral fracture parameter, including a discussion of the theoretical basis and practical aspects of its use for fracture predictions. Several examples illustrate the performance of the methods.
Mathematics Subject Classification ID: 74S05
Mathematics Subject Classification ID: 74R99
zbMATH DE Number: 1084148
zbMATH Keywords: crack growth prediction
reviewed by: N. F. F. Ebecken
MaRDI profile type: Publication
full work available at URL: s004660050184
OpenAlex ID: W2614154310
DOI: 10.1007/S004660050184
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label: 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
description: scientific article; zbMATH DE number 1084148