In this work the mechanical behaviour of CFRP laminates having an artificial wrinkle introduced in the critical section has been studied in the Open Hole Tension and Open Hole Compression configuration. The experimental test allowed determining the failure mechanism and the knockdown of the ultimate strength in five different configurations
9 Pages, 8 figures, submitted to Composite Science and Technology May 2013If carbon fibre layers are...
Following the general trend in the aviation sector, aerospace turbine engine manufacturers are maki...
The use of mechanical fasteners is still main assembling method for CFRP sub-structures in aircrafts...
With the wide adoption of composite materials for a variety of applications, the prediction of their...
MSc degree in Wind Energy at DTU in Denmark, and MSc degree in Aerospace Engineering at TU Delft in ...
Wrinkles are known to have a strong knock-down on the mechanical performance of structures made from...
Out-of-plane fibre waviness or ‘wrinkle’ defects significantly reduce the strength of laminated comp...
AbstractThe use of cost efficient CFRP materials is growing especially in the automotive application...
AbstractA critical parameter in a hybrid CFRP/steel composites is the shear stress between CFRP plie...
Composite pressure vessels (CPVs) have become the main equipment for hydrogen storage; however, the ...
AbstractThis paper provides an experimental investigation into the pin loading effects on the crack ...
The work presents a numerical and experimental analysis of a full-scale fatigue test on a CFRP rear ...
AbstractPresented is a numerical modeling analysis of the stress-strain behavior of composite overwr...
Wrinkle defects can be formed during the production of wind turbine blades consisting of composite m...
© 2014 Elsevier B.V. All rights reserved. To determine the amount of deformation resulting from fibr...
9 Pages, 8 figures, submitted to Composite Science and Technology May 2013If carbon fibre layers are...
Following the general trend in the aviation sector, aerospace turbine engine manufacturers are maki...
The use of mechanical fasteners is still main assembling method for CFRP sub-structures in aircrafts...
With the wide adoption of composite materials for a variety of applications, the prediction of their...
MSc degree in Wind Energy at DTU in Denmark, and MSc degree in Aerospace Engineering at TU Delft in ...
Wrinkles are known to have a strong knock-down on the mechanical performance of structures made from...
Out-of-plane fibre waviness or ‘wrinkle’ defects significantly reduce the strength of laminated comp...
AbstractThe use of cost efficient CFRP materials is growing especially in the automotive application...
AbstractA critical parameter in a hybrid CFRP/steel composites is the shear stress between CFRP plie...
Composite pressure vessels (CPVs) have become the main equipment for hydrogen storage; however, the ...
AbstractThis paper provides an experimental investigation into the pin loading effects on the crack ...
The work presents a numerical and experimental analysis of a full-scale fatigue test on a CFRP rear ...
AbstractPresented is a numerical modeling analysis of the stress-strain behavior of composite overwr...
Wrinkle defects can be formed during the production of wind turbine blades consisting of composite m...
© 2014 Elsevier B.V. All rights reserved. To determine the amount of deformation resulting from fibr...
9 Pages, 8 figures, submitted to Composite Science and Technology May 2013If carbon fibre layers are...
Following the general trend in the aviation sector, aerospace turbine engine manufacturers are maki...
The use of mechanical fasteners is still main assembling method for CFRP sub-structures in aircrafts...
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