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.006a" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.006a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Computational domain with boundary conditions</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="632387.fig.006b" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.006b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Model with cross sections</td></tr></table></td></tr></table>

<table>Computational domain and model cross sections.</table>

Modelling and Simulation in Engineering

fig6

Figure 6

Figure 6: Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method 