Fatigue-crack growth in two aluminum alloys and crack-closure analyses under constant-amplitude and spectrum loading-Reference-Cited by-同舟云学术

Fatigue-crack growth in two aluminum alloys and crack-closure analyses under constant-amplitude and spectrum loading

Published:2019-04 Issue: Volume:100 Page:307-318
ISSN:0167-8442
Container-title:Theoretical and Applied Fracture Mechanics
language:en
Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Newman J.C.,Walker K.F.

Funder

Australian Defence Science and Technology Group

National Research Council of Canada

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference34 articles.

1. Fatigue crack growth in 7249–T76511 aluminum alloy under constant-amplitude and spectrum loading;Newman;Fatigue Fract. Eng. Mater. Struct.,2015

2. J. Lamas, M. Edwards, P-3C Service Life Assessment Program – Full-Scale Fatigue Test. International Committee on Aeronautical Fatigue, 22nd Symposium, Lucerne, Switzerland, 2003.

3. Bharat Shah, P-3C Service Life Management, United States Air Force, Aircraft Structural Integrity Program (ASIP) Conference, Memphis, TN, USA, 2004.

4. Standard test method for measurement of fatigue crack growth rates, ASTM E-647-15, Volume 3.01 – Metals Test Methods and Analytical Procedure, 2018, pp. 714–762.

5. Compression pre-cracking to generate near threshold fatigue-crack-growth rates in two aluminum alloys;Newman;Int. J. Fatigue,2005

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