Delamination in the form of cracking or separation between plies in an advanced fiber composite laminate is a problem of major concern. Both advanced analytical methods and advanced computational analyses are conducted to: (1) develop an asymptotic solution for a composite laminate subject to out-of-plane bending; (2) construct advanced singular finite elements in conjunction with the development of nonsingular elements for this bending problem; and (3) evaluate the delamination failure mechanics parameters and the subsequent modes of fracture. A parametric study was also conducted to evaluate the influences of various lamination parameters on the delaminated composites
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
The use of advanced carbon fibre-reinforced composites in aircraft primary structures has been stead...
Based on theories of laminate anisotropic elasticity and interlaminar fracture, the complete solutio...
Delamination is a predominant failure mode in continuous fiber reinforced laminated composite struct...
A shear deformation model was developed to analyze local delaminations growing from transverse crack...
An equation was derived for the strain energy release rate, G, associated with local delamination gr...
The fundamental mechanics of delamination in fiber composite laminates is studied. Mathematical form...
Delamination is the most commonly observed failure mode in composite rotorcraft dynamic components. ...
A two-dimensional hybrid stress finite element analysis is described which was used to study the loc...
Delamination failure in a unidirectional curved composite laminate was investigated. The curved lami...
Fracture mechanics has been found to be a useful tool for understanding composite delamination. Anal...
This paper reviews our understanding of the influence of delamination on the fracture sequence and f...
Delamination is a common failure mode of laminated composite materials. This type of failure frequen...
This is a final report that summarizes the results achieved under this grant. The first major accomp...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
The use of advanced carbon fibre-reinforced composites in aircraft primary structures has been stead...
Based on theories of laminate anisotropic elasticity and interlaminar fracture, the complete solutio...
Delamination is a predominant failure mode in continuous fiber reinforced laminated composite struct...
A shear deformation model was developed to analyze local delaminations growing from transverse crack...
An equation was derived for the strain energy release rate, G, associated with local delamination gr...
The fundamental mechanics of delamination in fiber composite laminates is studied. Mathematical form...
Delamination is the most commonly observed failure mode in composite rotorcraft dynamic components. ...
A two-dimensional hybrid stress finite element analysis is described which was used to study the loc...
Delamination failure in a unidirectional curved composite laminate was investigated. The curved lami...
Fracture mechanics has been found to be a useful tool for understanding composite delamination. Anal...
This paper reviews our understanding of the influence of delamination on the fracture sequence and f...
Delamination is a common failure mode of laminated composite materials. This type of failure frequen...
This is a final report that summarizes the results achieved under this grant. The first major accomp...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
The use of advanced carbon fibre-reinforced composites in aircraft primary structures has been stead...