Thermo-Structural Behaviour Prediction of the Nose Cap of a Hypersonic Vehicle Based on Multifield Coupling

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Ma</td><td class="align_center">Altitude (km)</td><td class="align_center">Temperature (K)</td><td class="align_center">Pressure (Pa)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">6</td><td class="align_center">20</td><td class="align_center">217</td><td class="align_center">5475</td></tr><tr><td class="align_left">7.5</td><td class="align_center">20</td><td class="align_center">217</td><td class="align_center">5475</td></tr><tr><td class="align_left">9</td><td class="align_center">20</td><td class="align_center">217</td><td class="align_center">5475</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Thermo-Structural Behaviour Prediction of the Nose Cap of a Hypersonic Vehicle Based on Multifield Coupling 