Aerodynamic Optimization Based on Continuous Adjoint Method for a Flexible Wing

<table class="table-group" id="tab1"><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">Span</td><td class="align_center">60 m</td></tr><tr><td class="align_left">Aspect ratio</td><td class="align_center">8.0</td></tr><tr><td class="align_left">Sweep (leading edge)</td><td class="align_center">17.2°</td></tr><tr><td class="align_left">Sweep (quarter chord)</td><td class="align_center">15.0°</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 1

Table 1: Aerodynamic Optimization Based on Continuous Adjoint Method for a Flexible Wing 