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Through thickness fatigue failure of fibre-reinforced composites

Published online by Cambridge University Press:  04 July 2016

M. R. Wisnom  and
M. I. Jones
M. R. Wisnom
Affiliation:
Department of Aerospace Engineering University of Bristol Bristol, UK
M. I. Jones
Affiliation:
Department of Aerospace Engineering University of Bristol Bristol, UK
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Abstract

Simple straight and curved beams of unidirectional glass-epoxy were tested in fatigue to investigate failure under overall interlaminar tension and shear combined with local stresses at cut plies. Similar behaviour was observed as under static loading, with overall and local stresses interacting to cause delamination. When normalised, all the results lay close to, or above, a line determined from previous tension tests on specimens with cut plies, suggesting that this could be used as the basis for through thickness fatigue strength calculations.

Type
Research Article
Information
The Aeronautical Journal , Volume 102 , Issue 1012 , February 1998 , pp. 83 - 88
Copyright
Copyright © Royal Aeronautical Society 1998 

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