A Modified Walker Model Dealing with Mean Stress Effect in Fatigue Life Prediction for Aeroengine Disks

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/mpe/volume-2018/5148278/figures/5148278.fig.001a.svgz" name="5148278.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Walker, FGH4095 600°C</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/mpe/volume-2018/5148278/figures/5148278.fig.001b.svgz" name="5148278.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Walker, GH4169 650°C</td></tr></table>

<div>Equivalent completely reversed stress amplitude versus fatigue life correlations by Walker model for the (a) FGH4095 superalloy (600°C) and (b) GH4169 superalloy (650°C).</div>

Mathematical Problems in Engineering

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Figure 1: A Modified Walker Model Dealing with Mean Stress Effect in Fatigue Life Prediction for Aeroengine Disks 