Computational framework for multiaxial fatigue life prediction of compressor discs considering notch effects

Author:

Liao Ding,Zhu Shun-Peng,Correia José A.F.O.,De Jesus Abílio M.P.,Calçada Rui

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

China Postdoctoral Science Foundation Funded Project

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference80 articles.

1. Probabilistic damage tolerance analysis on turbine disk through experimental data;Hu;Eng Fract Mech,2012

2. Probabilistic Physics of Failure-based framework for fatigue life prediction of aircraft gas turbine discs under uncertainty;Zhu;Reliab Eng Syst Saf,2016

3. Probabilistic fatigue life prediction and reliability assessment of a high pressure turbine disc considering load variations;Zhu;Int J Damage Mech,2018

4. Fatigue reliability assessment of turbine discs under multi-source uncertainties;Zhu;Fatigue Fract Eng Mater Struct,2018

5. Structural reliability analysis and uncertainties-based collaborative design and optimization of turbine blades using surrogate model;Meng;Fatigue Fract Eng Mater Struct,2018

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