Fracture analysis of compressor blade of a helicopter engine-Reference-Cited by-同舟云学术

Fracture analysis of compressor blade of a helicopter engine

Published:2009-07 Issue:5 Volume:16 Page:1616-1622
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Witek L.,Wierzbińska M.,Poznańska A.

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference16 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. Fatigue strength of gas turbine compressor blades;Troshchenko;Eng Fail Anal,2000

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