Numerical Calculations on the Unsteady Aerodynamic Force of the Tilt-Rotor Aircraft in Conversion Mode

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/2147068/figures/2147068.fig.0026a.svgz" name="2147068.fig.0026a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Position 1, 0.3R</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/2147068/figures/2147068.fig.0026b.svgz" name="2147068.fig.0026b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Position 2, 0.6R</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/2147068/figures/2147068.fig.0026c.svgz" name="2147068.fig.0026c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Position 3, 0.9R</td></tr></table>

<div>Pressure distributions on wing locations at different tilt angles.</div>

International Journal of Aerospace Engineering

fig26

Figure 26

Figure 26: Numerical Calculations on the Unsteady Aerodynamic Force of the Tilt-Rotor Aircraft in Conversion Mode 