Residual strength of aircraft panels with multiple site damage

DOI10.1007/BF00350230zbMath0789.73057MaRDI QIDQ1315902

Li Chen, Robert Greif, Pin Tong

Publication date: 20 June 1994

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

zbMATH Keywords

stress intensity factorscrack tipsstress concentration factorshybrid finite element methodairframe structuremultiple cracks rivet load

Mathematics Subject Classification ID

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

Related Items (2)

Approximate method for stress intensity factors determination in case of multiple site damage ⋮ Analytical prediction of crack coalesce in multiple site damaged structures

Cites Work

• A hybrid finite element method for damage tolerance analysis
• ORTHOGONAL POLYNOMIAL SOLUTIONS TO SOME MIXED BOUNDARY-VALUE PROBLEMS IN ELASTICITY THEORY

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