Optimising fatigue crack growth predictions for small cracks under variable amplitude loading-Reference-Cited by-同舟云学术

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Optimising fatigue crack growth predictions for small cracks under variable amplitude loading

Published:2024-08 Issue: Volume:185 Page:108339
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Dixon B.,Fayek H.,Hodgen C.^ORCID,Wiley T.^ORCID,Barter S.^ORCID

Funder

Royal Australian Air Force

Publisher

Elsevier BV

Reference48 articles.

1. The practical need for short fatigue crack growth rate models;Main;Int J Fatigue,2021

2. Typical fatigue-initiating discontinuities in metallic aircraft structures;Barter;Int J Fatigue,2012

3. The lead crack fatigue lifing framework;Molent;Int J Fatigue,2011

4. Department of Defense Joint Service Specification Guide, Aircraft Structures. JSSG-2006, U.S. Department of Defense; 1998.

5. Department of Defense Standard Practice - Aircraft Structural Integrity Program. MIL-STD-1530D, U.S. Department of Defense; 2016.

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