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A numerical study on the thermal expansion coefficients of fiber

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37<br />

The area covered by a strain gauge is usually quite small, 1-5 mm, and this means<br />

that it samples <strong>the</strong> local behavior ra<strong>the</strong>r than <strong>the</strong> l<strong>on</strong>ger range average. In composites<br />

which have homogeneous reinforcement, such as flat laminates, unidirecti<strong>on</strong>al<br />

reinforcements and particulate composites, <strong>the</strong> technique can be used reliably, but<br />

cauti<strong>on</strong> needs to be exercised with woven structures. The active part <strong>of</strong> <strong>the</strong> strain<br />

gauge needs to cover several representative reinforcement units for <strong>the</strong> results to be<br />

representative <strong>of</strong> bulk material behavior.<br />

3.4 Theoretical C<strong>on</strong>siderati<strong>on</strong><br />

Micromechanics is a <str<strong>on</strong>g>study</str<strong>on</strong>g> <strong>of</strong> mechanical properties <strong>of</strong> composites in terms <strong>of</strong><br />

those <strong>of</strong> c<strong>on</strong>stituent materials (Tsai, & Hahn 1980). In discussing composite<br />

properties it is important to define a volume element which is small enough to show<br />

<strong>the</strong> microscopic structural details, yet large enough to represent <strong>the</strong> overall behavior<br />

<strong>of</strong> <strong>the</strong> composite. Such a volume element is called <strong>the</strong> representative volume<br />

element. A simple representative volume element can c<strong>on</strong>sist <strong>of</strong> a <strong>fiber</strong> embedded in<br />

matrix block.<br />

Once a representative volume element is chosen, proper boundary c<strong>on</strong>diti<strong>on</strong>s are<br />

prescribed. Ideally, <strong>the</strong>se boundary c<strong>on</strong>diti<strong>on</strong>s must represent <strong>the</strong> in situ states <strong>of</strong><br />

stress and strain within <strong>the</strong> composite. That is, <strong>the</strong> prescribed boundary c<strong>on</strong>diti<strong>on</strong>s<br />

must be <strong>the</strong> same as those if <strong>the</strong> representative volume element were actually in <strong>the</strong><br />

composite.<br />

Finally, a predicti<strong>on</strong> <strong>of</strong> composite properties follows from <strong>the</strong> soluti<strong>on</strong> <strong>of</strong> <strong>the</strong><br />

forgoing boundary value problem. Although <strong>the</strong> procedure involved is c<strong>on</strong>ceptually<br />

simple, <strong>the</strong> actual soluti<strong>on</strong> is ra<strong>the</strong>r difficult. C<strong>on</strong>sequently, many assumpti<strong>on</strong>s and<br />

approximati<strong>on</strong>s have been introduced, and <strong>the</strong>refore, various soluti<strong>on</strong>s are available.<br />

General assumpti<strong>on</strong>s in micromechanics <strong>of</strong> composites are:

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