Research Article

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

Table 3

Main geometric parameters for the two simulated specimens of turbine disk.

Parameters

Bolt-hole specimen/mm3.0/8.2512.034.5113.04.06.0
Run-way hole specimen/mm3.24.28.2511.234.2126.44.06.0