AbstractThe numerical analysis of engineering structures is usually based upon the assumptions of a homogeneous as well as a continuous medium. These simplifications are maintained also for structures made of fibre reinforced composite materials which possess by definition a heterogeneous finescale architecture. Furthermore in the course of the loading of such structures void nucleations might arise out of the debonding of the embedded fibres or the growth of microcracks inside the matrix phase. Hence, the assumption of a continuous and homogeneous medium is not valid from a microscopical point of view. Nevertheless, it is numerically advantageous to keep up these simplifying assumptions on the macrolevel. Therefore, the knowledge of the so...
A user's guide for the program gmc.f is presented. The program is based on the generalized method of...
The application of fiber reinforced laminated composite structures has been increasing steadily in ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83576/1/AIAA-2010-2693-128.pd
AbstractThe numerical analysis of engineering structures is usually based upon the assumptions of a ...
AbstractThe simultaneous twoscale analysis of unidirectionally fiber reinforced composite structures...
International audienceThis work is concerned with the modeling of ductile damage behavior in composi...
Abstract This work is concerned with the modeling of ductile damage behavior in composite materials ...
Abstract Failure induced by fiber microbuckling is a frequent failure mode in continuous fiber-reinf...
AbstractAn analysis of the effects of microscopic instabilities on the homogenized response of heter...
A critical issue in the micromechanics-based analysis of composite structures becomes the availabili...
peer-reviewedFibre reinforced composites exhibit a gradual damage accumulation to failure, with a m...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...
AbstractThe recent High Fidelity Generalized Method of Cells (HFGMC) micromechnical modeling framewo...
Micromechanics based models are considered for application to viscoelasticity and damage in metal ma...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97057/1/AIAA2012-1539.pd
A user's guide for the program gmc.f is presented. The program is based on the generalized method of...
The application of fiber reinforced laminated composite structures has been increasing steadily in ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83576/1/AIAA-2010-2693-128.pd
AbstractThe numerical analysis of engineering structures is usually based upon the assumptions of a ...
AbstractThe simultaneous twoscale analysis of unidirectionally fiber reinforced composite structures...
International audienceThis work is concerned with the modeling of ductile damage behavior in composi...
Abstract This work is concerned with the modeling of ductile damage behavior in composite materials ...
Abstract Failure induced by fiber microbuckling is a frequent failure mode in continuous fiber-reinf...
AbstractAn analysis of the effects of microscopic instabilities on the homogenized response of heter...
A critical issue in the micromechanics-based analysis of composite structures becomes the availabili...
peer-reviewedFibre reinforced composites exhibit a gradual damage accumulation to failure, with a m...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...
AbstractThe recent High Fidelity Generalized Method of Cells (HFGMC) micromechnical modeling framewo...
Micromechanics based models are considered for application to viscoelasticity and damage in metal ma...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97057/1/AIAA2012-1539.pd
A user's guide for the program gmc.f is presented. The program is based on the generalized method of...
The application of fiber reinforced laminated composite structures has been increasing steadily in ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83576/1/AIAA-2010-2693-128.pd