Advanced Aerostructural Optimization Techniques for Aircraft Design

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td align="left">State</td><td align="center">Mach</td><td align="center">Altitude, (Km)</td><td align="center">Lift coefficient</td><td align="center">Load factor</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td align="left">Cruise</td><td align="center">0.60</td><td align="center">20</td><td align="center">0.55</td><td align="center">1.0</td></tr><tr><td align="left">Maneuver</td><td align="center">0.60</td><td align="center">10</td><td align="center">0.326</td><td align="center">2.5</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

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Table 6

Table 6: Advanced Aerostructural Optimization Techniques for Aircraft Design 