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

<table class="table-group" id="tab7"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Background: no droop nose</td><td class="align_center">40,077,177 nodes</td></tr><tr><td class="align_left">Background: with droop nose</td><td class="align_center">72,109,161 nodes</td></tr><tr><td class="align_left">Flaps</td><td class="align_center">3,484,746 nodes</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Sizes of the different chimera grids used for 3D CFD performance evaluation.</div>

International Journal of Aerospace Engineering

tab7

Table 7

Table 7: Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose 