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.hindawi.com/articles/ijae/volume-2015/706915/figures/706915.fig.003a.svgz" name="706915.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Definition of GC and IP</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/706915/figures/706915.fig.003b.svgz" name="706915.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Interpolation to IP</td></tr></table>

<div>The immersed boundary method (IBM) using an image point (IP) based on a ghost cell (GC).</div>

International Journal of Aerospace Engineering

fig3

Figure 3

Figure 3: Cartesian Mesh Linearized Euler Equations Solver for Aeroacoustic Problems around Full Aircraft 