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

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Background/main airfoil</td><td class="align_center">123,377 nodes</td></tr><tr><td class="align_left">Flap</td><td class="align_center">17,936 nodes</td></tr><tr><td class="align_left">Total</td><td class="align_center">141,313 nodes</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Grid dimensions for the 2D CFD performance evaluation using chimera technique.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose 