Lift Augmentation on a Tiltrotor Wing Using the Combination of Vortex Generators and Gurney’s Flap

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/6646817/figures/6646817.fig.005a.svgz" name="6646817.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Lift coefficients</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/6646817/figures/6646817.fig.005b.svgz" name="6646817.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Drag coefficients</td></tr></table>

<div>Comparison of aerodynamic coefficients of a NACA 0012 airfoil with a 2% chord GF.</div>

International Journal of Aerospace Engineering

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Figure 5

Figure 5: Lift Augmentation on a Tiltrotor Wing Using the Combination of Vortex Generators and Gurney’s Flap 