Investigation of New Design Principles for the Centrifugal Compressor Vaned Diffusers

<table class="table-group" id="tab7"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Case</td><td class="align_center">Rel. <i>δ</i></td><td class="align_center">Rel. m</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left"><i>Baseline</i></td><td class="align_center">1</td><td class="align_center">1</td></tr><tr><td class="align_left"><i>Case11</i></td><td class="align_center">1.009</td><td class="align_center">1.003</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Performance comparisons for diffusers with different thicknesses.</div>

International Journal of Aerospace Engineering

tab7

Table 7

Table 7: Investigation of New Design Principles for the Centrifugal Compressor Vaned Diffusers 