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first is to calculate the shear <strong>an</strong>gle using the theoretical equation based on the kinematic<br />

<strong>an</strong>alysis of the bias-extension test. The second is to draw straight lines along the yarns<br />

for various images from the bias test. The third method is to use a series of images<br />

obtained from the test along with soft image correlation software. However, all these<br />

approaches carried out by the above researchers c<strong>an</strong>not be used for the woven<br />

composite that is wrapped round the pipe. The only way to measure the shear <strong>an</strong>gle,<br />

strain <strong>an</strong>d others due to thermal exp<strong>an</strong>sion is to apply Mohr‘s Circle theory using a<br />

strain gauge <strong>an</strong>d surface temperature detector.<br />

5.6 Summary <strong>an</strong>d Conclusions<br />

From the above results, from this experimental approach of using the surface<br />

temperature detector, it is possible to measure the CTE of the test material on site<br />

provided the measurement is carried out at proper locations; it also provides <strong>an</strong><br />

alternative method to the bonded temperature sensor which may involve extra cost <strong>an</strong>d<br />

time. For unreachable locations, for example, between layers of the composite repair,<br />

the temperature sensor has to be bonded next to the bonded strain gauge so that more<br />

accurate readings c<strong>an</strong> be obtained. From these experimental results also, it c<strong>an</strong> be<br />

concluded that the CTE measurement using this simple approach produced is acceptable<br />

<strong>an</strong>d practical in this composite based pipeline repair. However, this approach produces<br />

better <strong>an</strong>d accurate result in the isotropic material (i.e. steel) th<strong>an</strong> in the <strong>an</strong>isotropic<br />

material (i.e. composite).<br />

The results of maximum thermal strain at both layers (fourth <strong>an</strong>d eight layers)<br />

show that the thermal strain is directly proportional to the temperature increase. In the<br />

investigation of shear strain in the thermal exp<strong>an</strong>sion experiment, the shear strain is<br />

found to be higher at the eighth layer (i.e. 172 microstrain) compared to the fourth layer<br />

of composite (i.e. 73.3 microstrain). However, at the eighth layer, the shear strain was<br />

nearly const<strong>an</strong>t as temperatures increased. Therefore, the CTE readings at C3 <strong>an</strong>d C4<br />

(both at the eighth layer) as illustrated in Figure 5.12, were much closer to each other if<br />

compared to C1 <strong>an</strong>d C2 (at the fourth layer) which were less apparent. This shows that<br />

190

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