Lift Enhancement of Tiltrotor Wing Using a Gurney Flap

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2022/1245484/figures/1245484.fig.005a.svgz" name="1245484.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Lift curves</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2022/1245484/figures/1245484.fig.005b.svgz" name="1245484.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Drag curves</td></tr></table>

<div>Aerodynamic coefficients of a NACA 0012 wing with different GFs.</div>

International Journal of Aerospace Engineering

fig5

Figure 5

Figure 5: Lift Enhancement of Tiltrotor Wing Using a Gurney Flap 