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Sustainable Construction A Life Cycle Approach in Engineering

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IFCC-2.0<br />

IFCC-1.0<br />

IFCC-1.5<br />

Figure 13: IFCC – Deflection at mid-span<br />

The curves above <strong>in</strong>dicate that the <strong>in</strong>itial load behaviour of the various beams was generally l<strong>in</strong>ear<br />

until the po<strong>in</strong>t where <strong>in</strong>itial crack<strong>in</strong>g started, show<strong>in</strong>g non-l<strong>in</strong>ear behaviour. Beam CM (no<br />

fibres) failed soon after the first crack, with poor levels of ductility. The rema<strong>in</strong><strong>in</strong>g test specimens<br />

exhibited better performance, as the beams cont<strong>in</strong>ued to deflect. This led to the post-peak<br />

descend<strong>in</strong>g portion of the load-deflection curves.<br />

3.2.1 Peak Load<br />

A substantial <strong>in</strong>crease <strong>in</strong> peak load is observed for all test specimens conta<strong>in</strong><strong>in</strong>g fibres (TFRC –<br />

IFCC) when compared to the control mix (CM). The fibres embedded <strong>in</strong> the matrix bridged the<br />

micro-cracks dur<strong>in</strong>g the elastic stage, and prevented crack propagation. Consequently, the matrix<br />

was able to support higher loads prior to failure. The highest peak load recorded was<br />

20.9kN, measured for IFCA-2.0. When compared to the load achieved by the control mix<br />

(13.8kN), this resulted <strong>in</strong> an <strong>in</strong>crease of 7.1kN.<br />

Figure 14: Peak Load – Effect of volume fraction<br />

85

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