Assessment of stable tearing on fatigue fracture surfaces-Reference-Cited by-同舟云学术

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Assessment of stable tearing on fatigue fracture surfaces

Published:2010-09 Issue:6 Volume:17 Page:1313-1327
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Ab Rahman Mohd Fairuz,Mohammed Reza D.,Yu Xiaobo,Liu Qianchu,Clark Graham

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference34 articles.

1. Why aircraft fail;Finlay;Mater Today,2002

2. Fractographic techniques for the assessment of aircraft component cracking;Goldsmith,1989

3. Analysis and interpretation of aircraft component defects using quantitative fractography;Goldsmith,1990

4. Byrnes R, Sharp PK, Goldsmith NT, Clark G. Modelling of stable tearing during fatigue crack growth of 7050 aluminium alloy. Defence Science and Technology Organisation DSTO, Technical Report DSTO-TR-1032, Victoria; 2000.

5. Recovery of the RAAF MB326H – the tale of an ageing trainer fleet;Clark,1997

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Predictive models for stable tearing crack growth due to overloading in fatigue;Fatigue & Fracture of Engineering Materials & Structures;2012-12-05

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