Research on the Fatigue Performance of TC6 Compressor Blade under the CCF Effect

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Blade disc</td><td class="align_center">Geometric size</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Inner diameter (mm)</td><td class="align_center">220</td></tr><tr><td class="align_left">Outer diameter (mm)</td><td class="align_center">354</td></tr><tr><td class="align_left">Thickness (mm)</td><td class="align_center">30</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Blade disc geometric description.</div>

International Journal of Aerospace Engineering

tab6

Table 6

Table 6: Research on the Fatigue Performance of TC6 Compressor Blade under the CCF Effect 