© 2019 Elsevier Ltd A method to predict the fatigue life and residual strength of fiber reinforced composites subjected to variable amplitude (VA) loadings was developed. Based on a recent two-parameter residual strength model for constant amplitude (CA) loadings and coupled with the “equivalent residual strength assumption” (ERSA) the method allows accounting for the cycle-by-cycle loading variability and to build on a solid foundation a numerical procedure for fatigue calculations under spectrum loadings. The responses of quasi-isotropic carbon/epoxy laminate subjected to ordered and random block loadings were first tested and the simulations revealed that the load order strongly impacts residual strength. Then the approach is extended to...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
International audienceShort Fiber Reinforced Composite (SFRC) structures exhibit multiple microstruc...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
The accurate modeling of the fatigue behavior of composite materials under constant amplitude (CA) c...
Because of the relatively large number of possible failure mechanisms in fibre reinforced composite ...
This paper discusses the effect of loading rate on the static strength and fatigue behavior of glass...
The most popular methods of characterizing a composite's fatigue properties and predicting its life ...
A statistical residual strength degradation model for composite materials has been devised in the pr...
The success in the use of composite materials requires apart from cost-effective manufacturing a wel...
This paper summarizes the principal features of composites' responses when subjected to constant amp...
A model describing the fatigue behavior of composite materials under variable loadings is presented....
Fatigue and residual strength data available in literature were modeled with a modified two-paramete...
Fatigue and residual strength data available in literature were modeled with a modified two-paramete...
Fatigue and residual strength data available in literature were modeled with a modified two-paramete...
International audienceShort Fiber Reinforced Composite (SFRC) structures exhibit multiple microstruc...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
International audienceShort Fiber Reinforced Composite (SFRC) structures exhibit multiple microstruc...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
The accurate modeling of the fatigue behavior of composite materials under constant amplitude (CA) c...
Because of the relatively large number of possible failure mechanisms in fibre reinforced composite ...
This paper discusses the effect of loading rate on the static strength and fatigue behavior of glass...
The most popular methods of characterizing a composite's fatigue properties and predicting its life ...
A statistical residual strength degradation model for composite materials has been devised in the pr...
The success in the use of composite materials requires apart from cost-effective manufacturing a wel...
This paper summarizes the principal features of composites' responses when subjected to constant amp...
A model describing the fatigue behavior of composite materials under variable loadings is presented....
Fatigue and residual strength data available in literature were modeled with a modified two-paramete...
Fatigue and residual strength data available in literature were modeled with a modified two-paramete...
Fatigue and residual strength data available in literature were modeled with a modified two-paramete...
International audienceShort Fiber Reinforced Composite (SFRC) structures exhibit multiple microstruc...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...
International audienceShort Fiber Reinforced Composite (SFRC) structures exhibit multiple microstruc...
The increased use of advanced composite materials on primary aircraft structure has brought back to ...