The fracture mechanics of fiber-reinforced materials differs radically from that of 'homogeneous' materials. The combination of high-strength, high-modulus, brittle fibers having significant scatter in strength levels with relatively low-strength, tow-stiffness matrices give rise to modes of interna
Modeling the remaining strength of structural composite materials subjected to fatigue
β Scribed by Nathan L. Post; John Bausano; Scott W. Case; John J. Lesko
- Publisher
- Elsevier Science
- Year
- 2006
- Tongue
- English
- Weight
- 245 KB
- Volume
- 28
- Category
- Article
- ISSN
- 0142-1123
No coin nor oath required. For personal study only.
β¦ Synopsis
One scheme for reliability-based design that is growing in popularity for civil and naval applications is the load and resistance factor design (LRFD). Our goal in this research is the development of a simulation to predict the remaining strength of structural composites subjected to variable fatigue loading and environmental exposure. The results of this simulation can then be used in LRFD to determine appropriate material ''knockdown'' factors for use in engineering design applications. The work so far focuses on modeling the response of the material to fatigue damage only. The proposed Monte-Carlo style simulation combines a phenomenological residual strength based life prediction model for composites materials with an empirical stiffness based damage accumulation model. This model is demonstrated using data for two glass reinforced vinyl-ester polymer composite systems. The analysis of these results has led to new insight into how the changes in mechanical properties of these materials exposed to fatigue loading can be modeled.
π SIMILAR VOLUMES
In this work the fatigue behaviour of the sandwich composite materials in three point bending has been studied. A stiffness reduction approach was adopted which was further based on the interpolation by the empirical functions of our test results, whose coefficients depends on the material propertie
The first ply failure in composite laminates are studied by 3-D fracture mechanic approach. The fracture model is based on a crack embedded in one of the inner layers. Numeriil results for the case of "angle ply" laminates are based on a general 3-D finite difference progtam. Stress intensi~ factor