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.009a" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.009a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>PIV measurement (left) and computation (right) at cross section <svg height="9.8625002" id="M37" style="vertical-align:-2.29482pt" version="1.1" viewbox="0 0 7.875 9.8625002" width="7.875" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,9.8625)">
<g transform="translate(72,-64.11)">
<text transform="matrix(1,0,0,-1,-71.95,66.45)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝑦</tspan>
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</svg></td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="632387.fig.009b" src="https://static.hindawi.com/articles/mse/volume-2012/632387/figures/632387.fig.009b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>PIV measurement (left) and computation (right) at cross section <svg height="7.375" id="M38" style="vertical-align:-0.17555pt" version="1.1" viewbox="0 0 7.9250002 7.375" width="7.9250002" xmlns="http://www.w3.org/2000/svg">
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<g transform="translate(72,-66.1)">
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<tspan style="font-size: 12.50px; " x="0" y="0">𝑧</tspan>
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<table>Mean velocity component in the freestream direction by Murayama et al. [<a href="/journals/mse/2012/632387/#B6">6</a>].</table>

Modelling and Simulation in Engineering

Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

Figure 9