Aerodynamic Optimization Based on Continuous Adjoint Method for a Flexible Wing

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Parameter</td><td class="align_center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Density</td><td class="align_center">2780 kg/m<sup>3</sup></td></tr><tr><td class="align_left">Modulus</td><td class="align_center">73.1 × 10<sup>9</sup> Pa</td></tr><tr><td class="align_left">Poisson ratio</td><td class="align_center">0.33</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

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Table 2

Table 2: Aerodynamic Optimization Based on Continuous Adjoint Method for a Flexible Wing 