A numerical study on the thermal expansion coefficients of fiber
A numerical study on the thermal expansion coefficients of fiber A numerical study on the thermal expansion coefficients of fiber
5 temperature dependence of the dimensional behavior which results from softening of the resin. The elastic solution achieved by Foye in 1968 employed the finite element method for the first time in the field of micromechanical analysis of unidirectional composites (Adams & Crane, 1984). This generalized plane strain
6 concentration from pure metal to pure ceramic, using the aluminum–silicon carbide composite as a model system. Particular attention was devoted to the effects of phase connectivity, since other geometrical factors such as the phase shape and particle distribution play a negligible role in affecting the overall coefficient of thermal expansion (CTE) of the composite. Islam et al. (2001) studied the linear thermal expansion coefficients of unidirectional composites systematically by the finite element method. Thermal expansion coefficients were first determined for composites with perfectly bonded interface between fiber and matrix. Results are compared with available experimental and analytical results. Next cracks caused by debonding along the fiber-matrix interface were studied to investigate the effects of interface cracking on the transverse thermal expansion coefficients. A combined experimental and
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- Page 25 and 26: 16 2.2.2.2 Carbon Fibers Carbon is
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5<br />
temperature dependence <strong>of</strong> <strong>the</strong> dimensi<strong>on</strong>al behavior which results from s<strong>of</strong>tening <strong>of</strong><br />
<strong>the</strong> resin.<br />
The elastic soluti<strong>on</strong> achieved by Foye in 1968 employed <strong>the</strong> finite element<br />
method for <strong>the</strong> first time in <strong>the</strong> field <strong>of</strong> micromechanical analysis <strong>of</strong> unidirecti<strong>on</strong>al<br />
composites (Adams & Crane, 1984). This generalized plane strain <str<strong>on</strong>g>study</str<strong>on</strong>g> included<br />
two <strong>fiber</strong> arrangements, separate and combined loading <strong>of</strong> five <strong>of</strong> <strong>the</strong> six comp<strong>on</strong>ents<br />
<strong>of</strong> stress, c<strong>on</strong>tours <strong>of</strong> stresses in <strong>the</strong> matrix around a <strong>fiber</strong>, determinati<strong>on</strong> <strong>of</strong><br />
unidirecti<strong>on</strong>al lamina composite properties and an evaluati<strong>on</strong> <strong>of</strong> <strong>the</strong> accuracy <strong>of</strong> <strong>the</strong><br />
various finite element models.<br />
Adams and Crane (1984) modeled a microscopic regi<strong>on</strong> <strong>of</strong> a unidirecti<strong>on</strong>al<br />
composite by finite element micromechanical analysis using generalized plane strain<br />
formulati<strong>on</strong>, but including l<strong>on</strong>gitudinal shear loading. Their analysis was capable <strong>of</strong><br />
treating elastic, transversely isotropic <strong>fiber</strong> materials, as well as isotropic,<br />
elastoplastic materials. They used <strong>the</strong> micromechanical analysis to predict <strong>the</strong><br />
stress/strain resp<strong>on</strong>se into <strong>the</strong> inelastic range <strong>of</strong> graphite-epoxy laminate. Their<br />
results were in excellent agreement with available experimental data.<br />
Some <strong>of</strong> analytical models are critically reviewed and compared with<br />
experimental measurements by Bowles and Tompkins (1989). For <strong>the</strong> most part,<br />
large discrepancies between <strong>the</strong> predicted values <strong>of</strong> <strong>the</strong> transverse CTE and <strong>the</strong> test<br />
data are observed, except for <strong>the</strong> model <strong>of</strong> Rosen and Hashin (1970). Bowles and<br />
Tompkins (1989) also c<strong>on</strong>ducted finite element calculati<strong>on</strong>s for two cell geometries,<br />
including doubly periodic square and hexag<strong>on</strong>al patterns, and showed that <strong>the</strong>ir<br />
results were in good agreement with <strong>the</strong> experimental values and with <strong>the</strong> Rosen-<br />
Hashin (1970) analysis. The soluti<strong>on</strong> for <strong>the</strong> periodic square pattern provides <strong>the</strong><br />
reference for <strong>the</strong> present investigati<strong>on</strong>.<br />
The <strong>the</strong>rmal expansi<strong>on</strong> resp<strong>on</strong>se <strong>of</strong> macroscopically isotropic metal–ceramic<br />
composites was studied through micromechanical modeling by Shen (1998). He<br />
carried out three-dimensi<strong>on</strong>al finite element analyses for <strong>the</strong> entire range <strong>of</strong> phase