Fatigue behavior of the aeronautical Al–Li (2198) aluminum alloy under constant amplitude loading-Reference-Cited by-同舟云学术

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Fatigue behavior of the aeronautical Al–Li (2198) aluminum alloy under constant amplitude loading

Published:2013-11 Issue: Volume:56 Page:95-105
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Alexopoulos Nikolaos D.,Migklis Evangelos,Stylianos Antonis,Myriounis Dimitrios P.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference35 articles.

1. Aluminium–lithium alloys;Lavernia;J Mater Sci,1987

2. Evolution of Al–Li base products for aerospace and space applications;Rioja;Metall Mater Trans A,2012

3. Recent development in aluminium alloys for aerospace applications;Heinz;Mater Sci Eng A,2000

4. A combined approach to microstructure mapping of an Al–Li AA2199 friction stir weld;Steuwer;Acta Mater,2011

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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