Numerical stress and crack initiation analysis of the compressor blades after foreign object damage subjected to high-cycle fatigue-Reference-Cited by-同舟云学术

Numerical stress and crack initiation analysis of the compressor blades after foreign object damage subjected to high-cycle fatigue

Published:2011-12 Issue:8 Volume:18 Page:2111-2125
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Witek Lucjan

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference21 articles.

1. Fatigue failure of a compressor blade;Lourenço;Eng Fail Anal,2008

2. Failure analysis of Ti6Al4V gas turbine compressor blades;Kermanpur;Eng Fail Anal,2008

3. Failure analysis of a set of compressor blades;Silveira;Eng Fail Anal,2008

4. Poznanska A, Sniezek M, Wierzbinska M. Pitting corrosion – main factor generating fracture of the compressor of aeroengine blades under operation. In: Proceedings of IX conference. Turbomachinery, Rzeszow; 2003 [in Polish].

5. Fracture analysis of compressor blade of a helicopter engine;Witek;Eng Fail Anal,2009

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