A study on the compressive strength of thick carbon fibre-epoxy laminates
By J. Lee, Constantinos Soutis. 2007
225 citations recorded by the source corpus.
Subfields: Mechanical Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/2767a4d0264148b4e4e5a40fba373a1fbdacccb0
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Mechanical Engineering
- Constantinos Soutis
- J. Lee
- S. Hallett
- Conor T. McCarthy
- Michael McCarthy
- M. Wisnom
- Ping Xu
- Pengfei Liu
In Mechanics of Materials
- S. Hallett
- M. Wisnom
- Constantinos Soutis
- Conor T. McCarthy
- Supratik Mukhopadhyay
- Mike I. Jones
- J. Lee
- Jinyang Zheng
Citations in the corpus
- Scaling Effects in Notched Composites (2010, background): “Results of unnotched scaled tests are also included for both tension [6] and compression [24].”
- Comparison of open hole tension characteristics of high strength glass and carbon fibre-reinforced composite materials (2008, background): “As such, a considerable literature exists on the damage characteristics of notched CFRP laminates [2-17].”
- Finite element analysis of burst pressure of composite hydrogen storage vessels (2009, background): “After performing the stiffness reduction on the failed composite elements, the stress redistributions lead to the stress concentrations on the neighbouring elements [31,32].”
- Thin ply composites: Experimental characterization and modeling of size-effects (2014, unknown): “Residual strains, fibre alignment and waviness, porosity and the amount of fibre clustering and resin rich zones tend to increase in larger and thicker structures, thus introducing another kind of size effect which is closely related to the production process [2,9,10].”
- Compressive failure of laminates containing an embedded wrinkle; experimental and numerical study (2015, background): “It is well known that high fibre volume-fraction composites fail in axial compression by the formation and broadening of a highly localised and strained zone called ‘kink band’[19].”
- Measuring the notched compressive strength of composite laminates : Specimen size effects (2008, methodology): “However, the 8mm thick specimen’s average strength is significantly lower than that of thinner specimens (drops about 29 % in going from 2mm to 8mm) due to matrix cracking introduced by thermal stresses during the specimen cutting process [15].”