Simulation of crack growth in the compressor blade subjected to resonant vibration using hybrid method-Reference-Cited by-同舟云学术

Simulation of crack growth in the compressor blade subjected to resonant vibration using hybrid method

Published:2015-03 Issue: Volume:49 Page:57-66
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

Reference23 articles.

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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. p. 439–46 [in Polish].

5. Fatigue crack propagation simulation in an aircraft engine fan blade attachment;Barlow;Int J Fatigue,2005

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