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.0010a" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.0010a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Narrow band</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="632387.fig.0010b" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.0010b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>1/3-octave band (experimental scale)</td></tr></table></td></tr></table>

<table>Comparison of SPL spectrum by experiment and computations.</table>

Modelling and Simulation in Engineering

fig10

Figure 10

Figure 10: Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method 