Fatigue crack growth properties of a GLARE3-5/4 fiber/metal laminate-Reference-Cited by-同舟云学术

Fatigue crack growth properties of a GLARE3-5/4 fiber/metal laminate

Published:1999-06 Issue:3 Volume:63 Page:253-272
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Takamatsu Tohru,Matsumura Takashi,Ogura Norio,Shimokawa Toshiyuki,Kakuta Yoshiaki

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference17 articles.

1. A new fatigue resistant material: aramid reinforced aluminum laminate (ARALL);Vogelesang,1981

2. Fatigue of aircraft materials and structures;Schijve,1992

3. Schijve J. Development of fiber-metal laminate, ARALL and GLARE, new fatigue resistant materials, Report LR-715, Faculty of Aerospace Eng., Delft University of Technology, The Netherlands 1993

4. Crack growth and residual strength characteristics of two grades of glass-reinforced aluminum ‘Glare’;Young;Composite Structures,1994

5. An experimental crack growth model for fiber/metal laminates;Toi,1995

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