Jonathan D Fuller
University of Bristol
24 Papers
47 Citations
Jonathan D Fuller is an academic researcher from University of Bristol. The author has contributed to research in topics: Delamination & Ultimate tensile strength. The author has an hindex of 9, co-authored 23 publications. Previous affiliations of Jonathan D Fuller include Engineering and Physical Sciences Research Council & Bristol and Bath Science Park.
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Papers
The use of composite materials in modern orthopaedic medicine and prosthetic devices: A review
Marc-S. Scholz,J.P. Blanchfield,L. D. Bloom,Broderick H. Coburn,M. Elkington,Jonathan D Fuller,M.E. Gilbert,S.A. Muflahi,M F Pernice,Steven Rae,James Trevarthen,Simon White,Paul M. Weaver,Ian P Bond +13 more
TL;DR: The use of fiber reinforced composite materials for biomedical purposes is reviewed in this paper, where the development of polymer composite materials has, in recent years, led to technological advances across a wide range of applications in modern orthopaedic medicine and prosthetic devices.
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Pseudo-ductility and damage suppression in thin ply CFRP angle-ply laminates
TL;DR: In this paper, an experimental study using a spread tow thin ply carbon-epoxy prepreg material with a cured ply thickness of 0.03 mm is presented, which shows that highly nonlinear stress-strain behavior can be achieved with angle-ply laminates, whilst suppressing the damage mechanisms that normally cause their premature failure.
152
19th International Conference on Composite Materials
Jonathan D Fuller,Michael R Wisnom +1 more
- 02 Aug 2013
76
Exploration of the potential for pseudo-ductility in thin ply CFRP angle-ply laminates via an analytical method
TL;DR: In this article, an analytical modelling method that incorporates matrix plasticity and reorientation of the fibres into a classical laminate analysis for the prediction of the in-plane response of thin ply angle-ply laminates was presented.
69
Combining fibre rotation and fragmentation to achieve pseudo-ductile CFRP laminates
TL;DR: In this paper, a metal-like stress-strain curve for a [ ± θ m / 0 n ] s laminate has been shown to be formed by the gradual fragmentation of unidirectional (0 ° ) plies.
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