Comparison of open hole tension characteristics of high strength glass and carbon fibre-reinforced composite materials

O’Higgins, Ronan M.; McCarthy, Michael A.; McCarthy, Conor T.

doi:10.1016/j.compscitech.2008.06.003

Cited by 137 publications

(83 citation statements)

References 24 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…The axial tensile tests were conducted on nothed and unnotched specimens at RT, 95 o C and 125 o C, the results are shown in Figure 5. For the unnotched specimens, the stress-strain curve is almost linear at RT, which is similar with CF/PPS [13] and GF/epoxy [9], indicating that the polymer chains are frozen and the matrix is brittle at this temperature.…”

Section: Stress Strain Relationshipssupporting

confidence: 54%

“…For the unnotched specimens, the specimens at RT failed in a brittle mode, which are characterized by fibre bundles fracture and little amount of delamination at the surface ply where a higher interlaminar stress usually presents [9]. Judging from the extent and degree of damage, the initial damage is generated from the free edge.…”

Section: Damage Patternsmentioning

confidence: 99%

“…Then the failure behavior of the notched specimen will be dominated by the damage around the hole due to the stress concentration. Reference [9][10][11] investigated the notched tensile behavior and gave a deep insight into damage progression in the vicinity of the hole. They observed that the inital damage generated from the edge of the hole, leading to a redistribution of stress.…”

Section: Introductionmentioning

confidence: 99%

See 2 more Smart Citations

Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications

Wang

Zhang

et al. 2017

MATEC Web Conf.

View full text Add to dashboard Cite

Abstract. The effect of temperature on the mechanical behavior of 8-H satin woven glass fabric/polyethylene sulfide (GF/PPS) was investigated in this paper. Static-tensile tests were both conducted on notched and unnotched specimens at typical temperatures (ambient, 95 o C and 125 o C) based on the glass transition temperatures (Tg) of the neat resin and composite, their strength and moduli were obtained and compared. The damage patterns of failed specimens of notched and unnotched were examined with the aid of high-definition camera and stereomicroscope. The results of stress-strain relationships showed that the slight nonlinearity of the curves were observed for these two specimens, which was associated with the plastic deformation of localized resin. The damage patterns of notched and unnotched specimens at different temperatures proved that damage and plastic deformation were two simultaneous mechanisms and it was prominent in the notched. It was the overstress accommodation mechanism that led to a relative high strength rentention for the notched and a reduction of the hole sensitivity. The results obtained in this paper indicated that GF/PPS can be used as secondary aircraft structures at elevated temperatures higher than its Tg.

show abstract

Section: Stress Strain Relationshipssupporting

confidence: 54%

Section: Damage Patternsmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications

Wang

Zhang

et al. 2017

MATEC Web Conf.

View full text Add to dashboard Cite

show abstract

“…The homogenised properties of the composite were found to show good agreement with the experimentally measured properties of [18]. A parametric study, in which the size of the generated microstructure was varied, was carried out and it was found that the elastic moduli converged for a microstructure window which has a side of length of approximately 20 times the fibre radius, which for this material is approximately half a ply thickness (i.e.…”

Section: Discussionmentioning

confidence: 66%

A combined experimental–numerical approach for generating statistically equivalent fibre distributions for high strength laminated composite materials

Vaughan

McCarthy

2010

Composites Science and Technology

Self Cite

203

140

View full text Add to dashboard Cite

“…Fig. 16 shows the specimen geometry of CFRP OHT with material properties given in Table 2 33 . The specimen is 300 mm long, 36 mm wide and the diameter of the hole is 6 mm.…”

mentioning

confidence: 99%

Micro/macro approach for prediction of matrix cracking evolution in laminated composites

Ghayour

Hosseini‐Toudeshky

Jalalvand

et al. 2015

Journal of Composite Materials

View full text Add to dashboard Cite

General rightsThis document is made available in accordance with publisher policies. Please cite only the published version using the reference above. Abstract A computational constitutive model is presented to predict matrix cracking evolution in laminates under in-plane loading. Transverse cracks are treated as separate discontinuities in the micro model which provides damage parameters for the macro model. Both micro and macro models are implemented using Finite Element Analysis (FEA); specifically ANSYS, avoiding limitation of analytical micro modeling. The computational cost of the micro model is limited to constructing a database (DB) of micro-model predictions a priori. The macromodel is simply a FEA discretization of the structure using plane stress or shell elements in ANSYS. The macro model queries the DB, which effectively becomes a constitutive model. The damage surfaces in the DB are obtained from the results of large number of finite element micro-scale (unit-cell) analyses. The proposed procedure is implemented in ANSYS as a usermaterial subroutine for transverse crack initiation and propagation in symmetric cross-ply and [0r/(s/0n]s laminates under in-plane loads. This method is also examined to study matrix crack evolution in tensile specimen with open hole and the results found to be in good agreement with available experimental data.

show abstract

Comparison of open hole tension characteristics of high strength glass and carbon fibre-reinforced composite materials

Cited by 137 publications

References 24 publications

Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications

Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications

A combined experimental–numerical approach for generating statistically equivalent fibre distributions for high strength laminated composite materials

Micro/macro approach for prediction of matrix cracking evolution in laminated composites

Contact Info

Product

Resources

About