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

<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">Maximum rotating speed (rpm)</td><td class="align_center">LCF load simulation value (N)</td><td class="align_center">LCF load modified value (N)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">11,320</td><td class="align_center">25,686</td><td class="align_center">28,255</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab7

Table 7

Table 7: Research on the Fatigue Performance of TC6 Compressor Blade under the CCF Effect 