Fatigue crack growth under corrosive environments of Ti-6Al-4V specimens produced by SLM-Reference-Cited by-同舟云学术

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Fatigue crack growth under corrosive environments of Ti-6Al-4V specimens produced by SLM

Published:2020-12 Issue: Volume:118 Page:104852
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Jesus J.S.,Borrego L.P.,Ferreira J.A.M.,Costa J.D.,Capela C.

Funder

European Regional Development Fund

Foundation for Science and Technology

MCTES

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference16 articles.

1. Additive manufacturing: technology, applications and research needs;Guo;Front. Mech. Eng.,2013

2. Additive layered manufacturing: sectors of industrial application shown through case studies;Petrovic;Int. J. Prod. Res.,2011

3. Characterization of titanium aluminide alloy components fabricated by additive manufacturing using electron beam melting;Murr;Acta Mater.,2010

4. R.A. Zavanelli, P.G.E. Henriques, I. Ferreira, J.M.D. de Almeida Rollo, Corrosion-fatigue life of commercially pure titanium and Ti-6Al-4V alloys in different storage environments, J. Prosthetic Dent., https://doi.org/10.1067/mpr.2000.108758.

5. On the mechanical behaviour of titanium alloy TiAl6V4 manufactured by selective laser melting: fatigue resistance and crack growth performance;Leuders;Int. J. Fatigue,2013

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1. Effect of post-processing on the corrosive behaviour of L-DED Ti-6Al-4V;Materials Letters;2024-10

2. Effect of Al content on the fracture toughness and deformation behavior of Ti-Al binary alloys;Materials Science and Engineering: A;2024-09

3. Fatigue and corrosion‐fatigue behavior of the β‐metastable Ti‐5Al‐5Mo‐5V‐3Cr alloy processed by laser powder bed fusion;Fatigue & Fracture of Engineering Materials & Structures;2024-08-10

4. Fatigue cracking behavior and life assessment of TC11 titanium alloy in very high cycle regime at two working temperatures;Engineering Failure Analysis;2024-08

5. Low-Cycle Corrosion Fatigue Deformation Mechanism for an α+β Ti-6Al-4V-0.55Fe Alloy;Metals;2024-06-17

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