Fatigue and fracture behaviour of (Al-Cu-Li) AA2198 under different ageing conditions-Reference-Cited by-同舟云学术

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Fatigue and fracture behaviour of (Al-Cu-Li) AA2198 under different ageing conditions

Published:2024-07 Issue: Volume:184 Page:108286
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Kermanidis Alexis T.^ORCID,Charalampidou Christina-Margarita,Goulas Ioannis,Skarvelis Panagiotis,Alexopoulos Nikolaos D.^ORCID

Funder

Hellenic Foundation for Research and Innovation

University of the Aegean

Publisher

Elsevier BV

Reference49 articles.

1. The evolution of al-li base products for aerospace and space applications;Rioja;Metall Mater Trans A,2012

2. Quasi-static strength, deformation, and Fracture behavior of aluminum-lithium alloys;Srivatsan,2013

3. Fatigue behavior of the aeronautical Al–Li (2198) aluminum alloy under constant amplitude loading;Alexopoulos;Int J Fatigue,2013

4. Effect of aging treatment on microstructures, tensile properties and intergranular corrosion behavior of Al–Cu–Li alloy;Lin;Mater Charact,2018

5. Effect of ageing time on strength and microstructures of an Al–Cu–Li–Zn–Mg–Mn–Zr alloy;Li;Mater Sci Eng A,2008

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