Effects of Fiber Length on Elastic Moduli of Randomly-Oriented Chopped-Fiber Composites

Effects of Fiber Length on Elastic Moduli of Randomly-Oriented Chopped-Fiber Composites
Author: CT. Sun
Publisher:
Total Pages: 14
Release: 1979
Genre: Composite materials
ISBN:

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Based on a composite-cylinder model with a short cylindrical fiber embedded in the center of a cylindrical matrix, the longitudinal Young's modulus and major Poisson's ratio of a unidirectional, short-fiber composite are found in terms of the fiber volume fraction and the tip-to-tip spacing of the fibers. The expressions obtained are then modified to account for the influence of volume fraction and aspect ratio of the fibers. These results, together with Christensen and Waals' normalized expressions, are used to calculate the Young's modulus and Poisson's ratio of a randomly-oriented chopped-fiber composite in terms of the fiber volume fraction and its aspect ratio. The theory developed is then applied to examine numerically the effects of fiber length on the Young's modulus and Poisson's ratio of short glass-fiber/polyester-resin composites. The results show that the Young's modulus of both unidirectional and randomly-oriented fiber composites are strongly dependent on the fiber length; so is the Poisson's ratio, though to a lesser degree.

Understanding and Predicting the Stress Relaxation Behavior of Short-Fiber Composites

Understanding and Predicting the Stress Relaxation Behavior of Short-Fiber Composites
Author: Numaira Obaid
Publisher:
Total Pages:
Release: 2018
Genre:
ISBN:

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The viscoelastic properties of short-fiber composites are complex and not well-understood. Previous experimental work has shown that the viscoelastic properties of short-fiber composites are affected by both elastic fibers and the matrix, which is baffling since elastic fibers do not exhibit any time-dependence of their own. The goal of this study was to understand why and how elastic fibers can alter time-dependent behavior when contained in a composite. In this thesis, conventional shear-lag theory was adapted to include a time-dependent matrix and a novel analytical model was used to predict the tensile relaxation modulus of short-fiber composites. The model highlighted the importance of incorporating both the time-dependent tensile modulus of the matrix as well as its time-dependent shear modulus. Investigations using the model showed that since stress transfer in a short-fiber composite occurs through interfacial shearing, the time-dependent shear modulus of the matrix results in time-varying stress transfer the fiber. Since the stress in the fiber is time-dependent, it exhibits an apparent stress relaxation stemming from the relaxing shear modulus of the matrix. The model predictions were validated using finite-element simulations and experimental data. Comparison to real data confirmed the hypothesis that the time-dependency observed in elastic fibers stemmed from the indirect time-dependency imposed by the time-varying stress transfer from the matrix. The model was also used to determine the effect of various parameters including fiber aspect ratio and fiber volume fraction. For the first time, a critical aspect ratio for viscoelasticity was introduced. This was defined as the aspect ratio at which the contribution to composite stress relaxation by the fiber is maximized. The effect of fiber orientation was also examined, and an analytical model was developed to predict the stress relaxation of composites containing randomly-oriented fibers. It was found that random orientation in the plane would shrink the effect of fibers by one-third of what would be observed in oriented composites. In the last part of the thesis, we investigated the strain rate-dependence of short fiber-reinforced foams. The study highlighted a potential area where knowledge of the stress relaxation behavior of the short-fiber composites could prove useful.

Analysis and Test Strategies for Stress Rupture in Unidirectional Continuous Fiber Composite Structures

Analysis and Test Strategies for Stress Rupture in Unidirectional Continuous Fiber Composite Structures
Author: Amy Elspeth Engelbrecht-Wiggans
Publisher:
Total Pages: 510
Release: 2017
Genre:
ISBN:

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Stress rupture is a catastrophic failure mode in continuous unidirectional fiber composites, such as those used in composite overwrapped pressure vessels (COPVs). COPVs are currently used mainly in aerospace applications, such as storing the reserve oxygen on the International Space Station. Indeed a carbon/epoxy COPV failure caused the September 2016 explosion of the SpaceX Falcon 9 rocket at Cape Canaveral, leading to more than a billion dollars of damage. Currently COPVs are used in relatively small numbers, but the day is rapidly approaching when they will be used in the millions in many aspects of daily life, particularly in automotive applications. My research seeks to better understand stress rupture and more accurately estimate the probability that a specific composite structure will fail in stress rupture. Prediction of a composite’s stress rupture behavior is heavily based on results from extensive testing, as there are not yet methods to predict a composite’s stress rupture behavior based on the component materials’ properties. Testing results in comparatively small datasets of accelerated test data, which then must be extrapolated to predict a failure probability for a the service life of interest. This dissertation shows that the method used to analyze these datasets is crucial to accurately estimating the probability of a stress rupture failure, and also presents a data analysis method with lower variance and MSE estimates than current ad-hoc industry methods. Furthermore this dissertation compares current stress rupture models and derives a new, micromechanical stochastic stress rupture model.

Accelerated Stress Rupture Lifetime Assessment for Fiber Composites

Accelerated Stress Rupture Lifetime Assessment for Fiber Composites
Author:
Publisher:
Total Pages: 17
Release: 1997
Genre:
ISBN:

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Objective was to develop a theoretical and experimental framework for predicting stress rupture lifetime for fiber polymer composites based on short-term accelerated testing. Originally a 3-year project, it was terminated after the first year, which included stress rupture experiments and viscoelastic material characterization. In principle, higher temperature, stress, and saturated environmental conditions are used to accelerate stress rupture. Two types of specimens were to be subjected to long-term and accelerated static tensile loading at various temperatures, loads in order to quantify both fiber and matrix dominated failures. Also, we were to apply state-of-the-art analytical and experimental characterization techniques developed under a previous DOE/DP CRADA for capturing and tracking incipient degradation mechanisms associated with mechanical performance. Focus was increase our confidence to design, analyze, and build long-term composite structures such as flywheels and hydrogen gas storage vessels; other applications include advanced conventional weapons, infrastructures, marine and offshore systems, and stockpile stewardship and surveillance. Capabilities developed under this project, though not completed or verified, are being applied to NIF, AVLIS, and SSMP programs.