Study on the fatigue life and damage accumulation of a compressor blade based on a modified nonlinear damage model
Author:
Affiliation:
1. State Key Laboratory of Engines; Tianjin University; Tianjin 300072 China
2. Renai College; Tianjin University; Tianjin 301636 China
Funder
Joint Funds of National Natural Science Foundation of China and Civil Aviation Administration Foundation of China
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12753/fullpdf
Reference35 articles.
1. Aero-engine turbine blade life assessment using the Neu/Sehitoglu damage model;Abdullahi;Int J Fatigue,2014
2. Failure analysis of an axial compressor first row rotating blades;Poursaeidi;Eng Fail Anal,2013
3. Simulation of fatigue failure in composite axial compressor blades;Li;Mater Des,2011
4. Detection and numerical analysis of the most efforted places in turbine blades under real working conditions;Sadowski;Comput Mater Sci,2012
5. Course of SN-curves especially in the high-cycle fatigue regime with regard to component design and safety;Sonsino;Int J Fatigue,2007
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