Stress intensity factors for surface cracks in single-edge notch bend specimen by a three-dimensional weight function method
Author:
Affiliation:
1. AVIC Beijing Institute of Aeronautical Materials; Beijing 100095 China
2. Department of Aerospace Engineering; Mississippi State University; Mississippi State MS 39762 USA
Funder
National Natural Science Foundation of China
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12458/fullpdf
Reference15 articles.
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3. Small-crack growth and fatigue life predictions for high-strength aluminum alloys. Part II: crack closure and fatigue analyses;Newman;Fatigue Fract. Eng. Mater. Struct.,2000
4. Fatigue and crack growth in 7050-T7451 aluminum alloy under constant- and variable-amplitude loading;Newman;J. Eng. Gas Turb. Power,2013
5. Ziegler , B. M. 2011 Fatigue and fracture testing and analysis on four engineering materials
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