Ultrasonic and Conventional Fatigue Endurance of Aeronautical Aluminum Alloy 7075-T6, with Artificial and Induced Pre-Corrosion

Ultrasonic and Conventional Fatigue Endurance of Aeronautical Aluminum Alloy 7075-T6, with Artificial and Induced Pre-Corrosion

Ultrasonic and conventional fatigue tests were carried out on the AISI-SAE AA7075-T6 aluminum alloy, in order to evaluate the effect of artificial and induced pre-corrosion. Artificial pre-corrosion was obtained by two hemispherical pitting holes of 500-μm diameter at the specimen neck section, mach...

Full description

Bibliographic Details
Main Authors: Ishvari F. Zuñiga Tello, Marijana Milković, Gonzalo M. Domínguez Almaraz, Nenad Gubeljak
Format: Article
Language:English
Published: MDPI AG 2020-08-01
Series:Metals
Subjects:
Al alloy 7075-T6
ultrasonic fatigue
artificial pits
pre-corrosion
crack initiation
Online Access:https://www.mdpi.com/2075-4701/10/8/1033

Internet

https://www.mdpi.com/2075-4701/10/8/1033

Similar Items