Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="632387.fig.002a" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.002a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Cube allocation</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="632387.fig.002b" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.002b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Cell distribution</td></tr></table></td></tr></table>

<table>Cube and cell distribution around an airfoil with BCM.</table>

Modelling and Simulation in Engineering

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Figure 2

Figure 2: Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method 