FATIGUE CRACK GROWTH BEHAVIOUR OF FIBRE-METAL LAMINATE GLARE-1 AND METAL LAMINATE 7475 WITH DIFFERENT BLUNT NOTCHES-Reference-Cited by-同舟云学术

FATIGUE CRACK GROWTH BEHAVIOUR OF FIBRE-METAL LAMINATE GLARE-1 AND METAL LAMINATE 7475 WITH DIFFERENT BLUNT NOTCHES

Published:1997-11 Issue:11 Volume:20 Page:1573-1584
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:

Author:

Papakyriacou M.,Schijve J.,Stanzl-Tschegg S. E.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.1997.tb01512.x/fullpdf

Reference11 articles.

1. G. Roebroeks 1991 Towards GLARE, the development of a fatigue insensitive and damage tolerant aircraft material Doctor Thesis Faculty of Aerospace Engineering, Delft University of Technology

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