Research Article

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

Table 4

The comparison of estimated results of each mean stress models versus experimental data for simulated specimens.

SpecimenExperimental fatigue livesMedian fatigue life Predicted fatigue lives
GoodmanMorrowSWTWalkerM. Walker

Bolt-hole specimen20546, 24287, 15746, 8689, 24644, 9601, 25162169772804735276132342027614976

Error/65.2%107.8%−22.0%19.4%−11.8%

Run-way hole specimen14572, 26378, 60050, 53267, 151668, 51627, 46216, 28838, 8079, 12174, 13368298671082348642195692101521188

Error/−63.8%62.9%−34.5%−29.6%−29.1%