Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-part I: experimentation and fractographic analysis-Reference-Cited by-同舟云学术

Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-part I: experimentation and fractographic analysis

Published:2016-10-27 Issue:5 Volume:40 Page:776-789
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; MK43 0AL Bedfordshire UK

2. Institute for Advanced Manufacturing, Department of Mechanical, Materials and Manufacturing Engineering; University of Nottingham; 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.12544/fullpdf

Reference53 articles.

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3. Paint and sealant removal process 2004

4. FAA airworthiness directives no. FAA-2005-20918 2006

5. Das , G. Kosai , M. Miller , M. 2007 Development of a method for damage tolerance analysis for scribe marks adjacent to fuselage longitudinal and circumferential splices

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