Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose

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547C213 587 217 598 226 604C236 612 262 617 304 617C371 617 429 604 474 576C554 529 592 439 592 336C592 176 505 36 319 36C246 36 213 55 213 131V547Z"></path></g></svg></span></td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Take-off</td><td class="align_center">+10%</td><td class="align_center">+2.5°</td><td class="align_center">-5%</td></tr><tr><td class="align_left">Landing</td><td class="align_center">+15%</td><td class="align_center">+5°</td><td class="align_center">Not relevant</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Aerodynamic performance improvements due to the morphing droop nose device.</div>

International Journal of Aerospace Engineering

tab8

Table 8

Table 8: Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose 