Experimental and theoretical studies of corrosion-induced mechanical properties degradation of aircraft 2024 aluminum alloy
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Reference20 articles.
1. Development of fibre metal laminates for advanced aerospace structures
2. Modeling the effects of prior exfoliation corrosion on fatigue life of aircraft wing skins
3. Transition from pitting to fatigue crack growth—modeling of corrosion fatigue crack nucleation in a 2024-T3 aluminum alloy
4. Initiation and shape development of corrosion-nucleated fatigue cracking
5. Fatigue modeling for aircraft structures containing natural exfoliation corrosion
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