A Consistency Test of Thickness and Loading Noise Codes Using Ffowcs Williams and Hawkings Equation

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left"> Description</td><td align="center"> Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left"> Head</td><td align="center"> 1 300 (m)</td></tr><tr><td align="left">Flow rate</td><td align="center"><span style="width: 64.737503px;"><svg height="17.1625" id="M83" style="vertical-align:-0.1638pt" version="1.1" viewbox="0 0 64.737503 17.1625" width="64.737503" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg></span></td></tr><tr><td align="left">Rotational speed</td><td align="center"> 34 560 (rpm)</td></tr><tr><td align="left">Specific speed</td><td align="center"> 29</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Aerodynamic characteristics at operating point.

Advances in Acoustics and Vibration

tab1

Table 1

Table 1: A Consistency Test of Thickness and Loading Noise Codes Using Ffowcs Williams and Hawkings Equation 