A comparison of damage tolerance behaviour of two different nickel base super alloys under a turbine standard spectrum loads
Author:
Publisher
Elsevier BV
Subject
General Medicine
Reference18 articles.
1. Stress ratio effects on small fatigue crack growth in Ti–6Al–4V;Caton;Int. J. Fatigue,2012
2. Effect of load ratio and maximum stress intensity on the fatigue threshold in Ti–6Al–4V;Boyce;Eng. Fract. Mech.,2001
3. Fatigue crack growth prediction under spectrum load sequence in an aluminum alloy by K*-RMS Approach;Manjunatha;Int. J. Damage Mech.,2008
4. P.C. Sree, D. Kujawski, A two-parameter fatigue crack growth correlation using ΔK and Kmax parameters, InASME International Mechanical Engineering Congress and Exposition(Vol. 46583, p. V009T12A033) (2014) American Society of Mechanical Engineers.
5. Fatigue and crack-growth behavior in a titanium alloy under constant-amplitude and spectrum loading;Newman;Eng. Fract. Mech.,2018
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1. Fatigue crack growth behavior of a nickel-based superalloy under turbine standard spectrum loads;International Journal of Fracture;2024-05-17
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