An analysis utilizing laminated plate theory is developed to calculate the strain energy release rate associated with local delaminations originating at off-axis, single ply, matrix cracks in laminates subjected to uniaxial loads. The analysis includes the contribution of residual thermal and moisture stresses to the strain energy released. Examples are calculated for the strain energy release rate associated with local delaminations originating at 90 degrees and angle-ply (non-90 degrees) matrix ply cracks in glass epoxy and graphite epoxy laminates. The solution developed may be used to assess the relative contribution of mechanical, residual thermal, and moisture stresses on the strain energy release rate for local delamination for a var...
A fracture mechanics damage methodology to predict edge delamination is described. The methodology a...
Delamination related fracture processes in composite materials are discussed. Thermal and moisture i...
Delamination is a predominant failure mode in continuous fiber reinforced laminated composite struct...
An equation was derived for the strain energy release rate, G, associated with local delamination gr...
Two different families of graphite/epoxy laminates with similar layups but different stacking sequen...
ABSTRACT: This paper presents the results of a buckling and postbuckling analysis and modeling of em...
Constant amplitude tension-tension fatigue tests were conducted on AS4/3501-6 graphite/epoxy (02/ th...
The effect of the stress-free edge on the growth of local delaminations initiating from a matrix cra...
A shear deformation model was developed to analyze local delaminations growing from transverse crack...
A simple delamination analysis method is presented here. It is based on a shear-type deformation the...
This study focused on characterizing matrix cracking and delamination behavior in multidirectional l...
Quasi-static tension tests were conducted on AS4/3501-6 graphite epoxy laminates. Dye penetrant enha...
Delamination growth in compressively loaded composite laminates was studied analytically and experim...
Abstract. Prior methods for calculating energy release rate in cracked laminates were extended to ac...
Prior methods for calculating energy release rate in cracked laminates were extended to account for ...
A fracture mechanics damage methodology to predict edge delamination is described. The methodology a...
Delamination related fracture processes in composite materials are discussed. Thermal and moisture i...
Delamination is a predominant failure mode in continuous fiber reinforced laminated composite struct...
An equation was derived for the strain energy release rate, G, associated with local delamination gr...
Two different families of graphite/epoxy laminates with similar layups but different stacking sequen...
ABSTRACT: This paper presents the results of a buckling and postbuckling analysis and modeling of em...
Constant amplitude tension-tension fatigue tests were conducted on AS4/3501-6 graphite/epoxy (02/ th...
The effect of the stress-free edge on the growth of local delaminations initiating from a matrix cra...
A shear deformation model was developed to analyze local delaminations growing from transverse crack...
A simple delamination analysis method is presented here. It is based on a shear-type deformation the...
This study focused on characterizing matrix cracking and delamination behavior in multidirectional l...
Quasi-static tension tests were conducted on AS4/3501-6 graphite epoxy laminates. Dye penetrant enha...
Delamination growth in compressively loaded composite laminates was studied analytically and experim...
Abstract. Prior methods for calculating energy release rate in cracked laminates were extended to ac...
Prior methods for calculating energy release rate in cracked laminates were extended to account for ...
A fracture mechanics damage methodology to predict edge delamination is described. The methodology a...
Delamination related fracture processes in composite materials are discussed. Thermal and moisture i...
Delamination is a predominant failure mode in continuous fiber reinforced laminated composite struct...