Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

<table>Computed mean velocity component in the horizontal direction at cross section <svg height="10.9125" id="M46" style="vertical-align:-0.17555pt" version="1.1" viewbox="0 0 47.650002 10.9125" width="47.650002" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,10.9125)">
<g transform="translate(72,-63.27)">
<text transform="matrix(1,0,0,-1,-71.95,63.5)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝑥</tspan>
<tspan style="font-size: 12.50px; " x="10.339981" y="0">=</tspan>
<tspan style="font-size: 12.50px; " x="22.380369" y="0">0</tspan>
<tspan style="font-size: 12.50px; " x="28.63187" y="0">.</tspan>
<tspan style="font-size: 12.50px; " x="31.75762" y="0">0</tspan>
</text>
</g>
</g>
</svg> (left: BACK_TEAR, right: BACK_SEAL).</table>

Modelling and Simulation in Engineering

fig17

Figure 17

Figure 17: Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method 