Mode II delamination resistance of composites reinforced with inclined Z-pins-Reference-Cited by-同舟云学术

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Mode II delamination resistance of composites reinforced with inclined Z-pins

Published:2016-03 Issue: Volume:94 Page:565-572
ISSN:0264-1275
Container-title:Materials & Design
language:en
Short-container-title:Materials & Design

Author:

M'membe Beene,Gannon Sam,Yasaee Mehdi,Hallett Stephen R.,Partridge Ivana K.

Funder

Rolls-Royce plc and the Engineering and Physical Sciences Research Council

Composites University Technology Centre at the University of Bristol

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference18 articles.

1. Review of Z-pinned composite laminates;Mouritz;Compos. A Appl. Sci. Manuf.,2007

2. Comparative study of the mode I and mode II delamination fatigue properties of z-pinned aircraft composites;Pegorin;Mater. Des.,2015

3. Experimental characterisation of mixed mode traction–displacement relationships for a single carbon composite Z-pin;Yasaee;Compos. Sci. Technol.,2014

4. Properties and failure mechanisms of z-pinned laminates in monotonic and cyclic tension;Chang;Compos. A Appl. Sci. Manuf.,2006

5. Experimental Study on Z pin bridging law by pull-out tests;Liu,2003

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