Effect of hygrothermal treatment on the tensile properties - ethesis ...
Effect of hygrothermal treatment on the tensile properties - ethesis ...
Effect of hygrothermal treatment on the tensile properties - ethesis ...
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The matrix <str<strong>on</strong>g>of</str<strong>on</strong>g> <strong>the</strong> untreated sample shows no damage. In c<strong>on</strong>trast, <strong>the</strong> <str<strong>on</strong>g>hygro<strong>the</strong>rmal</str<strong>on</strong>g>ly<br />
treated samples show damage in <strong>the</strong>ir matrix. A crack is formed at <strong>the</strong> fibre-matrix,<br />
which leads to deb<strong>on</strong>ding at <strong>the</strong> interface, and finally fibre pullout occurs.<br />
100 0 C<br />
Fig. 4.8: Fibre regi<strong>on</strong> <str<strong>on</strong>g>of</str<strong>on</strong>g> untreated and 16 hours <str<strong>on</strong>g>hygro<strong>the</strong>rmal</str<strong>on</strong>g>ly treated sample<br />
The untreated samples do not show any sign <str<strong>on</strong>g>of</str<strong>on</strong>g> fibre pull-out. The failure <str<strong>on</strong>g>of</str<strong>on</strong>g> <strong>the</strong><br />
composite may be attributed to <strong>the</strong> failure <str<strong>on</strong>g>of</str<strong>on</strong>g> matrix. There are some signs <str<strong>on</strong>g>of</str<strong>on</strong>g> fibre<br />
breakage in <strong>the</strong> above figure in <strong>the</strong> case <str<strong>on</strong>g>of</str<strong>on</strong>g> <str<strong>on</strong>g>hygro<strong>the</strong>rmal</str<strong>on</strong>g>ly c<strong>on</strong>diti<strong>on</strong>ed samples.<br />
Mositure adsorbed <strong>on</strong>to <strong>the</strong> matrix and fibre can be seen.<br />
Fig. 4.9: Matrix cracking <str<strong>on</strong>g>of</str<strong>on</strong>g> untreated and 16 hours <str<strong>on</strong>g>hygro<strong>the</strong>rmal</str<strong>on</strong>g>ly treated sample<br />
The failure in case <str<strong>on</strong>g>of</str<strong>on</strong>g> 100 0 C hot pressed samples is due to matrix cracking. The loss<br />
<str<strong>on</strong>g>of</str<strong>on</strong>g> toughness due to complete curing <str<strong>on</strong>g>of</str<strong>on</strong>g> <strong>the</strong> unsaturated polyester resin doesn’t provide<br />
enough time for <strong>the</strong> transfer <str<strong>on</strong>g>of</str<strong>on</strong>g> load from matrix to fibre. The matrix behaves as a<br />
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