Thermal Fatigue Failure of Low-Pressure Turbine Blade in a Low-Bypass Turbofan Engine-Reference-Cited by-同舟云学术

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Thermal Fatigue Failure of Low-Pressure Turbine Blade in a Low-Bypass Turbofan Engine

Published:2019-03-18 Issue:2 Volume:19 Page:301-307
ISSN:1547-7029
Container-title:Journal of Failure Analysis and Prevention
language:en
Short-container-title:J Fail. Anal. and Preven.

Author:

Mishra R. K.,Jha S. K.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Safety, Risk, Reliability and Quality,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/s11668-019-00622-0.pdf

Reference25 articles.

1. B.A. Cowles, High cycle fatigue in aircraft gas turbines—an industry perspective. Int. J. Fract. 80, 147–163 (1996)

2. H. Ozaltun et al., An energy-based method for uni-axial fatigue life calculation. ASME Turbo Expo 2009: Power for Land, Sea, and Air. American Society of Mechanical Engineers (2009)

3. E. Poursaeidi, M. Aieneravaie, M.R. Mohammadi, Failure analysis of a second stage blade in a gas turbine engine. J. Eng. Fail. Anal. 15(8), 1111–1129 (2008)

4. J. Hour, B.J. Wicks, R.A. Antoniou, An investigation of fatigue failures of turbine blades in a gas turbine engine by mechanical analysis. J. Eng. Fail. Anal. 9(2), 201–211 (2002)

5. S. Suresh, Fatigue of Materials, 2nd edn. (Cambridge University Press, Cambridge, 2003), pp. 256–257

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of Turbine Blade Failure in a Turboprop Engine: A Case Study;Journal of Failure Analysis and Prevention;2022-01-18

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