Cartesian Mesh Linearized Euler Equations Solver for Aeroacoustic Problems around Full Aircraft

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/706915/figures/706915.fig.0014a.svgz" name="706915.fig.0014a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>DLR-F6 configuration</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/706915/figures/706915.fig.0014b.svgz" name="706915.fig.0014b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>OWN configuration</td></tr></table>

<div>Computational domains for the fuselage-wing-nacelle configurations (black dot: origin of coordinate system).</div>

International Journal of Aerospace Engineering

fig14

Figure 14

Figure 14: Cartesian Mesh Linearized Euler Equations Solver for Aeroacoustic Problems around Full Aircraft 