The high strength/stiffness-to-weight ratio that composite materials exhibit has led to the utilization of composites as alternative to traditional materials in weight-critical applications. However, the highly anisotropic nature of composites renders the strength prediction under complex loading challenging. To efficiently predict the failure of composite structures especially in cases where out-of-plane stresses are dominant, the modeling of damage onset and propagation plays an essential role in accurate strength predictions.Firstly, in this Thesis work the analysis of a composite L-profile, which is loaded such that significant out-of-plane stresses are generated in the curved region, is conducted. However, the inherent heterogeneity at...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...
The high strength/stiffness-to-weight ratio that composite materials exhibit has led to the utilizat...
The high strength/stiffness-to-weight ratio that composite materials exhibit has led to the utilizat...
In design with composite materials, the capability of tailoring the properties of the structure with...
Composite materials have a complex behavior, which is difficult to predict under different types of ...
Considerable effort has been put into the development of models describing damage and failure of fib...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
Composite materials are used more and more in aerospace, commercial and industrial applications due ...
Fibre reinforced polymers are progressively substituting metallic materials in many aerospace struct...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
To reduce development and certification costs for composite aircraft structures, efficient computati...
The thesis focuses on composite ribs of an airliner wing. The sizing factor for the composite ribs ...
This PhD thesis is the results of a three-year work aimed at improving the knowledge on the micromec...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...
The high strength/stiffness-to-weight ratio that composite materials exhibit has led to the utilizat...
The high strength/stiffness-to-weight ratio that composite materials exhibit has led to the utilizat...
In design with composite materials, the capability of tailoring the properties of the structure with...
Composite materials have a complex behavior, which is difficult to predict under different types of ...
Considerable effort has been put into the development of models describing damage and failure of fib...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
Composite materials are used more and more in aerospace, commercial and industrial applications due ...
Fibre reinforced polymers are progressively substituting metallic materials in many aerospace struct...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
To reduce development and certification costs for composite aircraft structures, efficient computati...
The thesis focuses on composite ribs of an airliner wing. The sizing factor for the composite ribs ...
This PhD thesis is the results of a three-year work aimed at improving the knowledge on the micromec...
In this thesis a constitutive model is developed for the numerical prediction of UD composite materi...
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...