Investigation and Improvement of Stall Characteristic of High-Lift Configuration without Slats

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td class="align_left">Wing section</td><td class="align_center">1</td><td class="align_center">2</td><td class="align_center">3</td><td class="align_center">4</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">Re<sub>L</sub> (×10<sup>6</sup>)</td><td class="align_center">13.60</td><td class="align_center">10.90</td><td class="align_center">9.00</td><td class="align_center">5.36</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Local Reynolds number of each wing section.</div>

International Journal of Aerospace Engineering

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Table 4

Table 4: Investigation and Improvement of Stall Characteristic of High-Lift Configuration without Slats 