Numerical Study on the Flow Mechanism of Compressor Rotor Blade Vibration under Different Inlet Probe Configurations

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Case</td><td class="align_center">Diameter</td><td class="align_center">Axial distance</td><td class="align_center">Circumferential position</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">1</td><td class="align_center">10 mm</td><td class="align_center">3.5R1</td><td class="align_center">0S</td></tr><tr><td class="align_left">2</td><td class="align_center">10 mm</td><td class="align_center">3.5R1</td><td class="align_center">0.5S</td></tr><tr><td class="align_left">3</td><td class="align_center">10 mm</td><td class="align_center">4.5R1</td><td class="align_center">0S</td></tr><tr><td class="align_left">4</td><td class="align_center">5 mm</td><td class="align_center">3.5R1</td><td class="align_center">0S</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Four different probe configurations under investigation.</div>

International Journal of Aerospace Engineering

tab3

Table 3

Table 3: Numerical Study on the Flow Mechanism of Compressor Rotor Blade Vibration under Different Inlet Probe Configurations 