Abstract
A physically-based damage model has been developed to predict the nonlinear behavior of cross-ply ceramic matrix laminates due to progressive failures. It has been shown to model the nonlinear stress-strain response of chemical vapor infiltrated (CVI) SiC/SiC composites under tension loading accurately. This model utilizes a consistent set of measurable material parameters as inputs and shows good agreement with measured tensile stress-strain curves for a variety of ply thickness ratios. The material model is also utilized to characterize the environmentally induced property degradation in CMC’s.
Volume Subject Area:
Durability and Damage Tolerance of Composites
Topics:
Ceramics,
Damage,
Laminates,
Modeling,
Composite materials,
Failure,
Stress,
Stress-strain curves,
Tension,
Vapors
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Copyright © 1997 by The American Society of Mechanical Engineers
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