Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-Part II: finite element analysis and prediction method-Reference-Cited by-同舟云学术

Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-Part II: finite element analysis and prediction method

Published:2016-11-10 Issue:6 Volume:40 Page:853-868
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Engng Mater Struct

Author:

Cini A¹²,Irving P E¹

Affiliation:

1. Damage Tolerance Group; Department of Materials, Cranfield University; College Road MK43 0AL Bedfordshire UK

2. Institute for Advanced Manufacturing; Department of Mechanical, Materials and Manufacturing Engineering University of Nottingham; University Park NG7 2RD Nottingham UK

Funder

Airbus

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12545/fullpdf

Reference48 articles.

1. Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-Part I: experimentation and fractographic analysis;Cini;Fatigue Fract. Eng. Mater. Struct,2016

2. Gallagher , J. P. Giessler , F. J. Berens , A. P. Engle , Jr. R. M. 1984 USAF damage tolerant design handbook: guidelines for the analysis and design of damage tolerant aircraft structures

3. Manning , S. D. Yang , J. N. 1984 USAF durability design handbook: guidelines for the analysis and design of aircraft structures

4. Manson , S. S. Hirschberg , M. H. 1967 Low cycle fatigue of notched specimens by consideration of crack initiation and propagation

5. Fatigue of metals under nonuniform stressed state. Part 1. Stresses state assessment methods and results of investigation;Troshchenko;Strength Mater.,2010

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