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Reliability-based low-cycle fatigue damage analysis for turbine blade with thermo-structural interaction

  • Published:2016-02 Issue: Volume:49 Page:289-300
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Gao Haifeng,Fei Chengwei,Bai Guangchen,Ding Lan

Funder

National Natural Science Foundation of China

Specialized Research Fund for the Doctoral Program of Higher Education of China

Innovation Foundation of BUAA for PhD Graduates

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. Analysis and prevention of turbine breakage in an engine starting motor;Yao;Mater. Mechan. Eng.,2002

2. Fracture failure analysis of high-pressure turbine blades of II stage;Liu;Heat Treat. Met.,2007

3. Failure analysis of gas turbine rotor blades;Kumari;Eng Fail. Anal.,2014

4. Common failures in gas turbine blades;Tim J.;Eng Fail. Anal.,2015

5. An improved procedure for component life estimation with applications;Rieger,1988

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