NUMERICAL TREATMENT OF DAMAGE PROPAGATION IN AXIALLY COMPRESSED COMPOSITE AIRFRAME PANELS

DOI10.1142/S0219455410003683zbMath1444.74016OpenAlexW2166204926MaRDI QIDQ3002022

Claudio Balzani, Werner Wagner

Publication date: 19 May 2011

Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0219455410003683

zbMATH Keywords

damage growthcomposite panelpostbuckling design

Mathematics Subject Classification ID

Material properties given special treatment (74E99)

Cites Work

• Elastoplastic finite element analysis of three-dimensional fatigue crack growth in aluminum shafts subjected to axial loading
• Computational modelling of impact damage in brittle materials
• Reduction of mesh sensitivity in continuum damage mechanics
• Finite element interface models for the delamination analysis of laminated composites: mechanical and computational issues
• Constitutive Equations for Damaging Materials
• Finite-deformation irreversible cohesive elements for three-dimensional crack-propagation analysis
• Interface element including point‐to‐surface constraints for three‐dimensional problems with damage propagation
• On the numerical integration of interface elements
• A Course on Damage Mechanics

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