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NASA NTRS ยท 20040191548

Computational Simulation of Composite Structural Fatigue

Abstract

Progressive damage and fracture of composite structures subjected to monotonically increasing static, tension-tension cyclic, pressurization, and flexural cyclic loading are evaluated via computational simulation. Constituent material properties, stress and strain limits are scaled up to the structure level to evaluate the overall damage and fracture propagation for composites. Damage initiation, growth, accumulation, and propagation to fracture due to monotonically increasing static and cyclic loads are included in the simulations. Results show the number of cycles to failure at different temperatures and the damage progression sequence during different degradation stages. 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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BibTeXRIS

Minnetyan, Levon. 2004-01-01. Computational Simulation of Composite Structural Fatigue. https://ntrs.nasa.gov/citations/20040191548

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