## 4 Results and Discussion
### Linear Static Finite Element Analysis Results
\begin{table}
\begin{tabular}{c c c c} \hline \hline  & \multicolumn{3}{c}{**Wing**} \\ \hline  & \multicolumn{3}{c}{**Transverse Bracing**} \\  & \multicolumn{3}{c}{**Bottom**} \\ \hline Size & \multicolumn{3}{c}{310 UC118} \\ Length (mm) & \multicolumn{3}{c}{3650} \\ Axis & \multicolumn{3}{c}{X} \\
1.35G & 48 & 19 \\
1.2G + 1.5Q & 64 & 20 \\
1.2G + \(Q+W_{orth}\) & 76 & 27 \\
1.2G + \(Q+W_{up}\) & 70 & 24 \\
1.2G + \(Q+W_{down}\) & 71 & 28 \\ \hline
**Maximum** & **76** & **28** \\
**Flexural Capacity** & **434** & **206** \\
**Utilisation** & **0.18** & **0.14** \\ \hline \hline \end{tabular} Notes: Bending moments are presented as absolute values.  
\end{table} 
Table 22: Analysis results of bending moments and member selection for wing component (kNm). \begin{table}
\begin{tabular}{c c c c} \hline \hline  & \multicolumn{3}{c}{**Wing**} \\ \hline  & \multicolumn{3}{c}{**Transs**} & \multicolumn{3}{c}{**Transverse Bracing**} \\  & \multicolumn{1}{c}{**Chord**} & \multicolumn{1}{c}{**Bracing**} & **Vertical** & **Bottom** \\ \hline Size & 200 UB29.8 & 100 UC14.8 & 100 UC14.8 & 310 UC118 \\ Length (mm) & 4327 & 4386 & 1600 & 3650 \\
1.35G & 619, \(-\)584 & 157, \(-\)174 & 129, \(-\)161 & 467, \(-\)1159 \\
1.2G + 1.5Q & 781, \(-\)675 & 231, \(-\)253 & 212, \(-\)112 & 581, \(-\)1172 \\
1.2G + \(Q+W_{orth}\) & 869, \(-\)707 & 203, \(-\)240 & 191, \(-\)154 & 633, \(-\)1366 \\
1.2G + \(Q+W_{up}\) & 862, \(-\)623 & 203, \(-\)235 & 185, \(-\)158 & 600, \(-\)1320 \\
1.2G + \(Q+W_{down}\) & 903, \(-\)651 & 204, \(-\)239 & 190, \(-\)184 & 623, \(-\)1360 \\ \hline
**Maximum** & **903, \(-\)707** & **231, \(-\)253** & **212, \(-\)184** & **633, \(-\)1366** \\
**Axial Capacity** & **1073, \(-\)1238** & **531, \(-\)612** & **531, \(-\)612** & **4214, \(-\)4590** \\
**Utilisation** & **0.84, 0.57** & **0.44, 0.41** & **0.40, 0.30** & **0.15, 0.30** \\ \hline \hline \end{tabular} Notes: 1 Compressive forces are shown as negative and tensile forces as positive. 2 Hanger transverse bracing employs AIS14410 high-tensile-strength round bars with tensile strength range of 850 to 1000 MPa and available diameter from 8 mm to 690 mm.  
\end{table} 
Table 21: Analysis results of axial forces and member selection for wing component (kN). \begin{table}
\begin{tabular}{c c c c} \hline \hline  & \multicolumn{3}{c}{**Wing**} \\ \hline  & \multicolumn{3}{c}{**Transverse Bracing**} \\  & \multicolumn{3}{c}{**Bottom**} \\ \hline Size & \multicolumn{3}{c}{310 UC118} \\ Length (mm) & \multicolumn{3}{c}{3650} \\ Axis & \multicolumn{3}{c}{X} \\
1.35G & 48 & 19 \\
1.2G + \(1.5Q\) & 64 & 20 \\
1.2G + \(Q+W_{orth}\) & 76 & 27 \\
1.2G + \(Q+W_{up}\) & 70 & 24 \\
1.2G + \(Q+W_{down}\) & 71 & 28 \\ \hline
**Maximum** & **76** & **28** \\
**Flexural Capacity** & **434** & **206** \\
**Utilisation** & **0.18** & **0.14** \\ \hline \hline \end{tabular} Notes: Bending moments are presented as absolute values.  
\end{table} 
Table 23: Analysis results of axial forces and member selection for substructure hanger component (kN). \begin{table}
\begin{tabular}{c c c c} \hline \hline \multicolumn{4}{c}{**Substructure Sub-Truss**} \\ \hline  & **Chord** & **Bracing** & **Vertical** \\ \hline Size & 150 UB14.0 & 150 UB14.0 & 150 UB14.0 \\ Length (mm) & 3859 & 1700 & 2000 \\
1.35G & 31, \(-\)39 & 1, 0 & 44, \(-\)33 \\
1.2G + 1.5Q & 26, \(-\)52 & 1, 0 & 59, \(-\)27 \\
1.2G + \(Q+W_{orth}\) & 18, \(-\)88 & 1, 0 & 101, \(-\)19 \\
1.2G + \(Q+W_{up}\) & 19, \(-\)75 & 7, \(-\)5 & 83, \(-\)19 \\
1.2G + \(Q+W_{down}\) & 18, \(-\)89 & 7, \(-\)5 & 104, \(-\)19 \\ \hline
**Maximum** & **31, \(-\)89** & **7, \(-\)5** & **104, \(-\)33** \\
**Axial Capacity** & **500, \(-\)577** & **500, \(-\)577** & **500, \(-\)577** \\
**Utilisation** & **0.06, 0.15** & **0.01, 0.01** & **0.21, 0.06** \\ \hline \hline \end{tabular} Note: Compressive forces are shown as negative and tensile forces as positive.  
\end{table} 
Table 26: Analysis results of axial forces and member selection for substructure sub-truss component (kN).