CFD Analysis of the Sideslip Angle Effect around a BWB Type Configuration

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4959265/figures/4959265.fig.0010a.svgz" name="4959265.fig.0010a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Side force coefficient</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4959265/figures/4959265.fig.0010b.svgz" name="4959265.fig.0010b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Rolling moment coefficient</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4959265/figures/4959265.fig.0010c.svgz" name="4959265.fig.0010c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Yawing moment coefficient</td></tr></table>

<div>Side force, rolling moment, and yawing moment coefficients for the side slip angle.</div>

International Journal of Aerospace Engineering

fig10

Figure 10

Figure 10: CFD Analysis of the Sideslip Angle Effect around a BWB Type Configuration 