Crack growth resistance curves of GLARE 3 5/4 0.3 fiber-metal laminates at low temperature-Reference-Cited by-同舟云学术

Crack growth resistance curves of GLARE 3 5/4 0.3 fiber-metal laminates at low temperature

Published:2014-08-11 Issue:3 Volume:38 Page:268-275
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Engng Mater Struct

Author:

Paiva Martins Fontes O. H.¹,Bastian F. L.¹,Castrodeza E. M.¹

Affiliation:

1. Laboratory of Fracture Mechanics, Department of Metallurgical and Materials Engineering; COPPE/Federal University of Rio de Janeiro; P.O. Box 68505 21941-972 Rio de Janeiro RJ Brazil

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12226/fullpdf

Reference16 articles.

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2. Historical overview

3. Fatigue properties of adhesive-bonded laminated sheet material of aluminum alloys;Schijve;Eng. Fract. Mech.,1979

4. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J. Mater. Process. Technol.,2000

5. Experimental techniques for fracture toughness determination of unidirectional fibre-reinforced metal laminates;Castrodeza;Fatigue Fract. Eng. Mater. Struct.,2002

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