An analytical method is presented for the estimation of compressive strength of delaminated composites. In the present method, the analysis of the delaminated composite is divided into three components: stress analysis of the laminate prior to the buckling of the sublaminate; eigenvalue analysis of the sublaminate; obtaining the compressive strength of the delaminated composite from these results. Based on this analytical method, the effect of location and size of delamination on damage tolerance has been studied on two types of plain weave fabric composites. Experimental study has been carried out on a typical plain weave E-glass/epoxy laminate GLE-12 with an artificially introduced delamination. A good correlation is observed between the ...
Delamination is a common form of damage that may develop during manufacture or service, causing degr...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
In cooperation with the Aircraft Strength Research Institute of the Chinese Aeronautical Establishme...
An efficient damage tolerance (DT) analysis method is required for application during the pre- limin...
An analytical model is presented for the compressive behaviour of plain weave fabric composites unde...
Damage tolerance is of critical importance to laminated composite structures. In this paper, we pres...
A recently developed fiber placement architecture, AP-PLY, has been shown to give significantly impr...
Abstract. Determination of levels of tolerance in delaminated composite panels is an important issue...
The theoretical and practical achievements in the field of the theory of strength and reliability of...
Layer composites reinforced with fabrics – laminates are construction materials in which mechanical ...
The use of advanced carbon fibre-reinforced composites in aircraft primary structures has been stead...
An analytical method is presented for the prediction of compressive strength at high strain rate loa...
[[abstract]]A one-dimensional model of delaminated laminates has been analyzed using a combination o...
The design and computation of laminated composite structures in terms of their strength is a complex...
Composite laminates are prone to delamination during hot pressing and cooling, this delamination is ...
Delamination is a common form of damage that may develop during manufacture or service, causing degr...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
In cooperation with the Aircraft Strength Research Institute of the Chinese Aeronautical Establishme...
An efficient damage tolerance (DT) analysis method is required for application during the pre- limin...
An analytical model is presented for the compressive behaviour of plain weave fabric composites unde...
Damage tolerance is of critical importance to laminated composite structures. In this paper, we pres...
A recently developed fiber placement architecture, AP-PLY, has been shown to give significantly impr...
Abstract. Determination of levels of tolerance in delaminated composite panels is an important issue...
The theoretical and practical achievements in the field of the theory of strength and reliability of...
Layer composites reinforced with fabrics – laminates are construction materials in which mechanical ...
The use of advanced carbon fibre-reinforced composites in aircraft primary structures has been stead...
An analytical method is presented for the prediction of compressive strength at high strain rate loa...
[[abstract]]A one-dimensional model of delaminated laminates has been analyzed using a combination o...
The design and computation of laminated composite structures in terms of their strength is a complex...
Composite laminates are prone to delamination during hot pressing and cooling, this delamination is ...
Delamination is a common form of damage that may develop during manufacture or service, causing degr...
The compressive strength of impact damaged composite laminates may be reduced by ply damage and dela...
In cooperation with the Aircraft Strength Research Institute of the Chinese Aeronautical Establishme...