NASA NTRS · 20080034820
Multi-Functional Composite Fatigue
Abstract
Damage and fracture of composites subjected to monotonically increasing static, tension-tension cyclic, pressurization, and flexural cyclic loading are evaluated via a recently developed composite mechanics code that allows the user to focus on composite response at infinitely small scales. Constituent material properties, stress and strain limits are scaled up to the laminate level to evaluate the overall damage and durability. Results show the number of cycles to failure at different temperatures. A procedure is outlined for use of computational simulation data in the assessment of damage tolerance, determination of sensitive parameters affecting fracture, and interpretation of results with insight for design decisions.
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Minnetyan, Levon, Chamis, Christos C.. 2008-09-09. Multi-Functional Composite Fatigue. https://ntrs.nasa.gov/citations/20080034820
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