Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="9"><hr/></td></tr><tr><td class="align_left">Fitting surface</td><td class="align_center">1</td><td class="align_center">2</td><td class="align_center">3</td><td class="align_center">4</td><td class="align_center">5</td><td class="align_center">6</td><td class="align_center">7</td><td class="align_center">8</td></tr><tr><td class="align_left">Gap size (mm)</td><td class="align_center">0.15</td><td class="align_center">0.15</td><td class="align_center">0.15</td><td class="align_center">0.15</td><td class="align_center">0</td><td class="align_center">0.1</td><td class="align_center">0.1</td><td class="align_center">0.25</td></tr><tr class="table-tr"><td colspan="9"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The defined initial gap sizes for the selected possible passageways.</div>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions 

Table 4 | Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions 