Fatigue behavior of an airfoil with tolerable exfoliation cracks induced by dynamic corrosion: Experimental and numerical assessment-Reference-Cited by-同舟云学术

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Fatigue behavior of an airfoil with tolerable exfoliation cracks induced by dynamic corrosion: Experimental and numerical assessment

Published:2024-09 Issue: Volume:163 Page:108567
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Cahue-Díaz D.,García-García V.^ORCID,Herrera-Sandoval N.D.,Tena-Martínez J.J.,Salazar-Torres J.A.

Funder

National Technology of Mexico

Publisher

Elsevier BV

Reference46 articles.

1. Aircraft Skin Corrosion and Structural Safety Considerations, De Securitate et Defensione;Pila;O Bezpieczeństwie i Obronności,2021

2. Corrosion-fatigue: a review of damage tolerance models;Larrosa;Int. Mater. Rev.,2018

3. Fatigue cracking from a corrosion pit in an aircraft bulkhead;Barter;Eng. Fail. Anal.,2014

4. Management of airframe in-service pitting corrosion by decoupling fatigue and environment;Molent;Corros. Mater. Degrad.,2021

5. The lead crack fatigue lifting framework;Molent;Int. J. Fatigue.,2011

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