Contact stress analysis and fatigue life prediction of turbine disc–blade attachment with fir‐tree tenon structure-Reference-Cited by-同舟云学术

Contact stress analysis and fatigue life prediction of turbine disc–blade attachment with fir‐tree tenon structure

Author:

Yuan Rong¹,Liao Ding²,Zhu Shun‐Peng²^ORCID,Yu Zheng‐Yong²,Correia José³,De Jesus Abilio³^ORCID

Affiliation:

1. School of Mechanical Engineering Chengdu University Chengdu China

2. School of Mechanical and Electrical Engineering University of Electronic Science and Technology of China Chengdu China

3. INEGI, Faculty of Engineering University of Porto Porto Portugal

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Guangzhou Municipal Science and Technology Project

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

Reference63 articles.

1. Key technology analysis of aeroengine structural reliability;Li D;Aeronaut Manuf Technol.,2016

2. Common characteristics in failure analysis of aeroengine blade;Li W;Gas Turbine Exp Res.,2002

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