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3.6 To determine other factors’ influences on the Numerical Model<br />

3.6.1 Introduction<br />

In this section, it is import<strong>an</strong>t to show that the developed numerical model that has<br />

been discussed in the previous section is the right <strong>an</strong>d suitable model to be used in the<br />

next stress <strong>an</strong>d strain distribution studies. There are two methods of validating this<br />

model. The first is to compare the numerical hoop <strong>an</strong>d axial stress values of the chosen<br />

model with several other models <strong>an</strong>d validate them <strong>an</strong>alytically. Details of this method<br />

are going to be discussed further in this section. The second method is to compare this<br />

chosen numerical model against the actual pipe specimen which has similar physical<br />

<strong>an</strong>d mech<strong>an</strong>ical properties, dimension <strong>an</strong>d geometry. This will be further explained <strong>an</strong>d<br />

discussed in a later chapter (i.e. experimental work). In this stress comparison study,<br />

which involves several models, what must be clearly addressed is that the defect <strong>an</strong>d<br />

nominal pipe thicknesses of each model remain const<strong>an</strong>t <strong>an</strong>d follow the actual test rig<br />

specifications.<br />

3.6.2 Comparison of Results<br />

As mentioned in the earlier section, in order to justify the preselected model (in<br />

this case Model 3) as the right <strong>an</strong>d most suitable model, the numerical results of hoop<br />

stress (S11) <strong>an</strong>d axial stress (S22) of each model from ABAQUS were obtained <strong>an</strong>d<br />

compared against the results of the m<strong>an</strong>ual calculation (<strong>an</strong>alytical method). A simple<br />

shell theory was applied in this m<strong>an</strong>ual calculation as shown below;<br />

For Hoop stress, σh (S11), it was referred to as Hoop Strain, εh (Kaminski, 2005) <strong>an</strong>d<br />

multiplied by Young‘s Modulus as shown below;<br />

<strong>an</strong>d,<br />

h<br />

PD<br />

4tE<br />

h = E. h<br />

(Equation 3.1)<br />

(Equation 3.2)<br />

74

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