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Cyclic crack growth behaviour of two nickel base turbine disc alloys
Date
1998-05-15
Author
Arslan, G
Doruk, M
Metadata
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The high temperature fatigue crack growth behaviour of the nickel base superalloys Alloy 718 and Rene 95 (specimen thickness = 4.1 mm) were investigated and compared with each other. Fatigue crack propagation (FCP) tests were carried out in laboratory air at room temperature and 600 degrees C by using C-T (compact tension) type specimen that were fatigue precracked at room temperature.
Subject Keywords
Temperature
URI
https://hdl.handle.net/11511/65471
Journal
JOURNAL OF MATERIALS SCIENCE
DOI
https://doi.org/10.1023/a:1004369622557
Collections
Department of Metallurgical and Materials Engineering, Article