Application of the Multiaxial Fatigue Life Prediction Model Suitable to the Key Components of Aeroengine Considering the Effect of Non‐Proportionality
['Junqi Feng', 'Dasheng Wei', 'Tonghui Wang', 'Xiyuan Zhang', 'Shun Yang']
/
Fatigue & Fracture of Engineering Materials & Structures
/ Vol. 49
/ No. 10
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