The smeared crack band theory is implemented within the generalized method of cells and high-fidelity generalized method of cells micromechanics models to capture progressive failure within the constituents of a composite material while retaining objectivity with respect to the size of the discretization elements used in the model. An repeating unit cell containing 13 randomly arranged fibers is modeled and subjected to a combination of transverse tension/compression and transverse shear loading. The implementation is verified against experimental data (where available), and an equivalent finite element model utilizing the same implementation of the crack band theory. To evaluate the performance of the crack band theory within a repeating u...
A new damage model based on a micromechanical analysis of cracked [+/- Theta/90n]s laminates subject...
A new multiscale micromechanical approach is developed for the prediction of the behavior of fiber r...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83576/1/AIAA-2010-2693-128.pd
The smeared crack band theory is implemented within the generalized method of cells and high-fidelit...
AbstractThe smeared crack band theory is implemented within the high-fidelity generalized method of ...
A continuum-level, dual internal state variable, thermodynamically based, work potential model, Scha...
A framework is presented that enables coupled multiscale analysis of composite structures. The recen...
Flow/damage surfaces can be defined in terms of stress, inelastic strain rate, and internal variable...
This paper presents a three-dimensional, energy based, anisotropic, stiffness reduction, progressive...
An efficient implementation of the generalized method of cells micromechanics model is presented tha...
A micromechanics analysis modeling method was developed to analyze the damage progression and fatigu...
The phenomenon of crack propagation is among the predominant modes of failure in many natural and en...
A mesh objective crack band model was implemented within the generalized method of cells micromechan...
A novel, multiscale mechanics model for predicting the evolution of damage and failure in continuous...
A computational micromechanics (CMM) model is employed to interrogate the assumptions of a recently ...
A new damage model based on a micromechanical analysis of cracked [+/- Theta/90n]s laminates subject...
A new multiscale micromechanical approach is developed for the prediction of the behavior of fiber r...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83576/1/AIAA-2010-2693-128.pd
The smeared crack band theory is implemented within the generalized method of cells and high-fidelit...
AbstractThe smeared crack band theory is implemented within the high-fidelity generalized method of ...
A continuum-level, dual internal state variable, thermodynamically based, work potential model, Scha...
A framework is presented that enables coupled multiscale analysis of composite structures. The recen...
Flow/damage surfaces can be defined in terms of stress, inelastic strain rate, and internal variable...
This paper presents a three-dimensional, energy based, anisotropic, stiffness reduction, progressive...
An efficient implementation of the generalized method of cells micromechanics model is presented tha...
A micromechanics analysis modeling method was developed to analyze the damage progression and fatigu...
The phenomenon of crack propagation is among the predominant modes of failure in many natural and en...
A mesh objective crack band model was implemented within the generalized method of cells micromechan...
A novel, multiscale mechanics model for predicting the evolution of damage and failure in continuous...
A computational micromechanics (CMM) model is employed to interrogate the assumptions of a recently ...
A new damage model based on a micromechanical analysis of cracked [+/- Theta/90n]s laminates subject...
A new multiscale micromechanical approach is developed for the prediction of the behavior of fiber r...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83576/1/AIAA-2010-2693-128.pd