Residual strength prediction for aircraft panels with multiple site damage, using the EPFEAM for stable crack growth analysis

DOI10.1007/BF00369780zbMath0825.73675MaRDI QIDQ1898444

C.-R. Pyo, Satya N. Atluri, Hiroshi Okada

Publication date: 29 October 1995

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

Mathematics Subject Classification ID

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

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Recent advances in the alternating method for elastic and inelastic fracture analyses

Cites Work

• Analysis of cracks in aging aircraft structures, with and without composite-patch repairs
• An analytical-numerical alternating method for elastic-plastic analysis of cracks
• Elasto‐plastic stress analysis. A generalization for various contitutive relations including strain softening
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