The effect of combined cycle fatigue upon the fatigue performance of TI–6AL–4V fan blade material
Author:
Publisher
Elsevier BV
Subject
Industrial and Manufacturing Engineering,Metals and Alloys,Computer Science Applications,Modelling and Simulation,Ceramics and Composites
Reference3 articles.
1. High cycle fatigue in aircraft as turbines—an industry perspective;Cowles;Int. J. Fatigue,1996
2. N.A. Fleck, R.A. Smith, A discussion of mechanisms for accelerated and retarded fatigue crack growth, in: Sixth International Conference on Fraction, Delhi, India, 1984, pp. 1832–1829.
3. Effect of load ratio and maximum stress intensity on the fatigue threshold in Ti–6Al–4V;Boyce;Eng. Fract. Mech,2001
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