Correlating stress ratio effects on the fatigue crack growth rate behavior of a nickel-based superalloy GTM718-Reference-Cited by-同舟云学术

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Correlating stress ratio effects on the fatigue crack growth rate behavior of a nickel-based superalloy GTM718

Published:2023-11 Issue: Volume: Page:
ISSN:2214-7853
Container-title:Materials Today: Proceedings
language:en
Short-container-title:Materials Today: Proceedings

Author:

Malipatil Sharanagouda G,Bojja Ramesh,Jagannathan N,Majila Anuradha N,Chandru Fernando D,Manjunatha CM

Publisher

Elsevier BV

Subject

Materials Science (miscellaneous)

Reference25 articles.

1. Fatigue crack growth prediction under spectrum load sequence in an aluminum alloy by K*-RMS approach;Manjunatha;Int. J. Damage Mech,2008

2. Prediction of fatigue crack growth after single overload in an aluminium alloy;Manjunatha;AIAA J.,2004

3. Experimental and numerical studies to estimate fatigue crack growth behaviour of Ni-based super alloy;Kumar;Theor. Appl. Fract. Mech.,2018

4. High-cycle fatigue of Ti-6Al-4V;Ritchie;Fatigue Fract. Eng. Mater. Struct.,1999

5. 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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