Advanced Design of a Full-Scale Active Morphing Droop Nose

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Maximum take-off weight</td><td class="align_center">32560 kg</td></tr><tr><td class="align_left">Maximum zero fuel weight</td><td class="align_center">31200 kg</td></tr><tr><td class="align_left">Cruise Mach at 20000 ft</td><td class="align_center">0.52</td></tr><tr><td class="align_left">Landing Mach at sea level</td><td class="align_center">0.197</td></tr><tr><td class="align_left">Mean aerodynamic chord</td><td class="align_center">2.565 m</td></tr><tr><td class="align_left">Reference wing area</td><td class="align_center">32.384 m<sup>2</sup></td></tr><tr><td class="align_left">Reference wing span</td><td class="align_center">14.827 m</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Reference aircraft characteristics.</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: Advanced Design of a Full-Scale Active Morphing Droop Nose 