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An Interface Damage Model for the Simulation of Delamination Under Variable-Mode Ratio in Composite Materials

National Aeronautics and Space Administration

Date: 2018 June 1
Document access: http://hdl.handle.net/2072/312148
Publisher: National Aeronautics and Space Administration
Rights: Tots els drets reservats
Subject: Materials laminats
Laminated materials
Materials compostos -- Deslaminatge
Composite materials -- Delamination
Materials compostos -- M猫todes de simulaci贸
Composite materials -- Simulation methods
Assaigs de materials
Materials -- Testing
Title: An Interface Damage Model for the Simulation of Delamination Under Variable-Mode Ratio in Composite Materials
Type: info:eu-repo/semantics/article
Repository: Recercat

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Authors