Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications-Reference-Cited by-同舟云学术

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Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications

Published:2005-09 Issue:3 Volume:8 Page:287-291
ISSN:1516-1439
Container-title:Materials Research
language:
Short-container-title:Mat. Res.

Author:

Rodrigues Elenice Maria¹,Matias Adalberto¹,Godefroid Leonardo Barbosa¹,Bastian Fernando Luiz²,Al-Rubaie Kassim S.³

Affiliation:

1. UFOP, Brazil

2. UFRJ, Brazil

3. EMBRAER, Brazil

Publisher

FapUNIFESP (SciELO)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Link

http://www.scielo.br/pdf/mr/v8n3/26039.pdf

Reference33 articles.

1. Fatigue crack closure under cyclic tension;Elber W;Engng Fract Mech,1970

2. A geometric model for fatigue crack closure induced by fracture surface morphology;Suresh S;Metall Trans,1982

3. Propagation of short fatigue cracks;Suresh S;Intl Metals Rev,1984

4. Fatigue Crack Growth Threshold Concepts: AIME (American Institute of Mining, Metallurgical and Petroleum Engineers);Suresh S,1984

5. Crack deflection: implications for the growth of long and short fatigue cracks;Suresh S;Metall Trans,1983

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