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The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination (2016)

First Author: Rhead A

Attributed to: Aerostructural Efficiency of Damage Tolerant Composites via Optimised Fibre Placement funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1017/s000192400000765x

Publication URI: http://dx.doi.org/10.1017/s000192400000765x

Type: Journal Article/Review

Parent Publication: The Aeronautical Journal

Issue: 1186

ISSN: 00019240