Fatigue Reliability Analysis System for Key Components of Aero-Engine

<table class="table-group" id="tab7"><tr><td><table class="table"><tr><td class="thead-hr" colspan="7"><hr/></td></tr><tr class="thead"><td class="align_left">Mode</td><td class="align_center">1st</td><td class="align_center">2nd</td><td class="align_center">3rd</td><td class="align_center">4th</td><td class="align_center">5th</td><td class="align_center">6th</td></tr><tr><td class="thead-hr" colspan="7"><hr/></td></tr><tr><td class="align_left">Frequency (Hz)</td><td class="align_center">508.65</td><td class="align_center">647.42</td><td class="align_center">2025.5</td><td class="align_center">2653.7</td><td class="align_center">4852.5</td><td class="align_center">5908.5</td></tr><tr class="table-tr"><td colspan="7"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Probe frequency calculation results.</div>

International Journal of Aerospace Engineering

tab7

Table 7

Table 7: Fatigue Reliability Analysis System for Key Components of Aero-Engine 