Fatigue damage development in new fibre metal laminates made by the VARTM process-Reference-Cited by-同舟云学术

Fatigue damage development in new fibre metal laminates made by the VARTM process

Published:2010-08-25 Issue:4 Volume:34 Page:240-249
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:

Author:

BAUMERT E. K.,JOHNSON W. S.,CANO R. J.,JENSEN B. J.,WEISER E. S.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.2010.01509.x/fullpdf

Reference25 articles.

1. Fibre Metal Laminates

2. Fracture toughness of 7075-T6 and - T651 sheet, plate and multilayered adhesive-bonded panels;Kaufman;J. Basic Eng.,1967

3. Effective remote stresses and stress intensity factors for an adhesive bonded multi-ply laminate;Johnson;Eng. Fract. Mech.,1977

4. A new fatigue resistant material: Aramid reinforced aluminum laminate (ARALL);Vogelesang;Proceedings of the 11th ICAF Symposium, Noordwijkerhout, The Netherlands. National Aerospace Laboratory, Amsterdam, The Netherlands,1981

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