Transition Effect on the Flow Dynamics in a Compressor Blade Passage

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Flow case</td><td class="align_center">A (mm)</td><td class="align_center">RMS (mm)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Ref-laminar</td><td class="align_center">4.37</td><td class="align_center">1.21</td></tr><tr><td class="align_left"><i>X</i>/<i>C</i> = 0.02</td><td class="align_center">4.73</td><td class="align_center">1.22</td></tr><tr><td class="align_left"><i>X</i>/<i>C</i> = 0.16</td><td class="align_center">3.64</td><td class="align_center">1.16</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>RMS of average shock oscillations and shock amplitude for flow cases with the microstep.</div>

Shock and Vibration

tab3

Table 3

Table 3: Transition Effect on the Flow Dynamics in a Compressor Blade Passage 