2005
DOI: 10.1016/j.compscitech.2004.12.028
|View full text |Cite
|
Sign up to set email alerts
|

Moisture sorption and mechanical degradation of VARTMed three-dimensional braided carbon–epoxy composites

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

1
14
0
2

Year Published

2006
2006
2018
2018

Publication Types

Select...
9

Relationship

0
9

Authors

Journals

citations
Cited by 30 publications
(19 citation statements)
references
References 20 publications
1
14
0
2
Order By: Relevance
“…Regardless of the fiber coating, wet composites were found to suffer from interfacial debonding, matrix craze, and fiber pullout with a subsequent decrease in mechanical properties. Decreased flexural strength, flexural modulus, and shear strength were also reported by Wan et al in three‐dimensional braided carbon‐epoxy laminates prepared by vacuum assisted resin transfer molding. In addition to these specific cases, the bulk of existing literature indicates a near universal consensus on the undesirable decrease in material properties due to absorbed moisture in polymers and their composites.…”
Section: Introductionsupporting
confidence: 75%
“…Regardless of the fiber coating, wet composites were found to suffer from interfacial debonding, matrix craze, and fiber pullout with a subsequent decrease in mechanical properties. Decreased flexural strength, flexural modulus, and shear strength were also reported by Wan et al in three‐dimensional braided carbon‐epoxy laminates prepared by vacuum assisted resin transfer molding. In addition to these specific cases, the bulk of existing literature indicates a near universal consensus on the undesirable decrease in material properties due to absorbed moisture in polymers and their composites.…”
Section: Introductionsupporting
confidence: 75%
“…plasticization, but it also attacks the fiber-matrix interface [143][144][145]. A reduction in strength and stiffness due to moisture absorption can be attributed to various damage mechanisms which can include matrix cracking, fibre/matrix interface, matrix plasticization/softening, stress generation due to swelling of the system, chemical degradation [122,138,139,146,147].…”
Section: Composite Materialsmentioning
confidence: 99%
“…Three-dimensional braided carbon fiber reinforced epoxy (C 3D /EP) composites are excellent materials for surgery or aviation because of their good properties, such as improved overall performance, high strength, desirable modulus, splendid friction and wear characteristics, etc [2,3]. The deposition of some coatings on the surface of C 3D /EP composites will be greatly helpful to their applications.…”
Section: Introductionmentioning
confidence: 99%