Development of Fibre Metal Laminates: concurrent multi-scale modeling and testing-Reference-Cited by-同舟云学术

Development of Fibre Metal Laminates: concurrent multi-scale modeling and testing

Published:2006-08-15 Issue:20 Volume:41 Page:6777-6788
ISSN:0022-2461
Container-title:Journal of Materials Science
language:en
Short-container-title:J Mater Sci

Author:

Sinke J.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/s10853-006-0206-5.pdf

Reference11 articles.

1. Vlot A, Glare (2001) History of the development of a new aircraft material. Kluwer Academic Publishers, The Netherlands

2. Alderliesten RC (1998) Development of an empirical crack growth model for Fibre Metal Laminates. Preliminary MSc Thesis, Delft University of Technology

3. Vermeulen B, van Tooren MJL, Peeters LJB (September 2005) Knowledge-based design method for fibre metal laminate fuselage panels. Int DETC conference, Long Beach, CA, USA

4. Alderliesten RC (2005) Fatigue crack propagation and delamination growth in glare. PhD Thesis, The Netherlands

5. Suiker ASJ, Fleck NA (2004) J Fatigue 125:1

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