This paper details a complete crush model for composite materials with focus on shear dominated crushing under a3D stress state. The damage evolution laws and nal failure strain conditions are based on data extracted from shearexperiments. The main advantages of the current model are: no need to measure the fracture toughness in shear andtransverse compression, mesh objectivity without the need for a regular mesh and nite element characteristic length, apressure dependency of the shear response, account for load reversal and for some orthotropic eects (making the modelsuitable for Non-Crimp Fabric composites). The model is validated against a range of relevant experiments, namely athrough-the-thickness compression specimen and a at crush co...
Crush tests have been performed on flat unidirectional non-crimp fabric (NCF) coupons with different...
This paper details the theory and implementation of a composite damage model, addressing damage with...
none4noDOI volume: 10.15651/978-88-9385-029-2In this work, the validation of the Finite Element (FE)...
This paper details a complete crush model for composite materials with focus on shear dominated crus...
This paper details a complete crush model for composite materials with focus on shear dominated crus...
A class of composite materials with fully 3D fibre-reinforcements have shown weight efficient streng...
A progressive damage model for matrix compression is complemented with matrix tension in a physicall...
In this paper, a practical orthotropic damage model is developed and tested for composite materials ...
Fibre reinforced polymers are progressively substituting metallic materials in many aerospace struct...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
The crushing response of fiber-reinforced composite structures under compressive loading is investig...
The high specific stiffness and strength of composites makes it advantageous for load carrying struc...
A material model which incorporates several key capabilities which have been identified by the aeros...
Crash modeling of composite structures remains limited in application and has not been effectively d...
A simple mathematical model for predicting the crushing stress of the composite materials is present...
Crush tests have been performed on flat unidirectional non-crimp fabric (NCF) coupons with different...
This paper details the theory and implementation of a composite damage model, addressing damage with...
none4noDOI volume: 10.15651/978-88-9385-029-2In this work, the validation of the Finite Element (FE)...
This paper details a complete crush model for composite materials with focus on shear dominated crus...
This paper details a complete crush model for composite materials with focus on shear dominated crus...
A class of composite materials with fully 3D fibre-reinforcements have shown weight efficient streng...
A progressive damage model for matrix compression is complemented with matrix tension in a physicall...
In this paper, a practical orthotropic damage model is developed and tested for composite materials ...
Fibre reinforced polymers are progressively substituting metallic materials in many aerospace struct...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
The crushing response of fiber-reinforced composite structures under compressive loading is investig...
The high specific stiffness and strength of composites makes it advantageous for load carrying struc...
A material model which incorporates several key capabilities which have been identified by the aeros...
Crash modeling of composite structures remains limited in application and has not been effectively d...
A simple mathematical model for predicting the crushing stress of the composite materials is present...
Crush tests have been performed on flat unidirectional non-crimp fabric (NCF) coupons with different...
This paper details the theory and implementation of a composite damage model, addressing damage with...
none4noDOI volume: 10.15651/978-88-9385-029-2In this work, the validation of the Finite Element (FE)...