Experimental investigation on damage evolution in pre-corroded aluminum alloy 7075-T7651 under fatigue loading-Reference-Cited by-同舟云学术

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Experimental investigation on damage evolution in pre-corroded aluminum alloy 7075-T7651 under fatigue loading

Published:2021-01 Issue: Volume:799 Page:140206
ISSN:0921-5093
Container-title:Materials Science and Engineering: A
language:en
Short-container-title:Materials Science and Engineering: A

Author:

Song Haipeng,Liu Changchun,Zhang Hao,Yang Xudong,Chen Yajun,Leen Sean B.

Funder

National Natural Science Foundation of China

Open Foundation of Jiangsu Province Key Laboratory of Aerospace Power System

Scientific Research Foundation of Civil Aviation University of China

Science Foundation Ireland

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference31 articles.

1. Recent developments in advanced aircraft aluminium alloys

2. In-situ SEM study of fatigue micro-crack initiation and propagation behavior in pre-corroded AA7075-T7651

3. Experimental and theoretical studies of corrosion-induced mechanical properties degradation of aircraft 2024 aluminum alloy

4. Managing airframe fatigue from corrosion pits – A proposal

5. Corrosion pit size distributions and fatigue lives—a study of the EIFS technique for fatigue design in the presence of corrosion

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3. Effect of corrosion pit on fatigue damage and failure in powder bed fusion AlSi10Mg;Fatigue & Fracture of Engineering Materials & Structures;2024-05-13

4. Corrosion pit-induced stress concentration in 7005 aluminium alloy: Mechanical degradation and pit parameter analysis;Engineering Fracture Mechanics;2024-05

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