Fatigue Reliability Analysis System for Key Components of Aero-Engine

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Working state</td><td class="align_center">Stress (MPa)</td><td class="align_center">Strain</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Ground idling</td><td class="align_center">692.67</td><td class="align_center">0.002752</td></tr><tr><td class="align_left">Cruising</td><td class="align_center">796.93</td><td class="align_center">0.003798</td></tr><tr><td class="align_left">Maximum continuous</td><td class="align_center">868.84</td><td class="align_center">0.005551</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Stress and strain results of three working states.</div>

International Journal of Aerospace Engineering

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Table 2

Table 2: Fatigue Reliability Analysis System for Key Components of Aero-Engine 