A non-linear model for in-plane shear damage and failure of composite laminates-Reference-Cited by-同舟云学术

A non-linear model for in-plane shear damage and failure of composite laminates

Published:2014-01 Issue:1-2 Volume:93 Page:17-24
ISSN:0365-7442
Container-title:Aerotecnica Missili & Spazio
language:en
Short-container-title:Aerotec. Missili Spaz.

Author:

Fanteria D.,Panettieri E.

Publisher

Springer Science and Business Media LLC

Link

http://link.springer.com/content/pdf/10.1007/BF03404672.pdf

Reference19 articles.

1. C. C. Chamis and J. W. Sinclair, “10° off-axis tensile test for intralaminar shear characterization of fiber composites”, NASA Tech. Note, No. NASA TN D-8215, April 1976.

2. ASTM, D4255/D4255M-01(2007), “Standard Test Method for In-Plane Shear Properties of Polymer Matrix Composite Materials by the Rail Shear Method”.

3. ASTM, D2344/D2344M-00(2006), “Standard Test Method for Short-Beam Strength of Polymer Matrix Composite Materials and Their Laminates”.

4. ASTM, D3518/D3518M-94(2007), “Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate”.

5. ASTM, D5379/D5379M-12, “Standard Test Method for Shear Properties of Composite Materials by the V-Notched Beam Method”.

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