A general purpose orthotropic elasto-plastic computational constitutive material model has been developed to improve predictions of the response of composites subjected to high velocity impact. The three-dimensional orthotropic elasto-plastic composite material model is being implemented initially for solid elements in LS-DYNA as MAT213. In order to accurately represent the response of a composite, experimental stress-strain curves are utilized as input, allowing for a more general material model that can be used on a variety of composite applications. The theoretical details are discussed in a companion paper. This paper documents the implementation, verification and qualitative validation of the material model using the T800-F3900 fiber/r...
A continuum damage model for the prediction of damage onset and structural collapse of structures ma...
This monograph is organized to look at: the successful application of composites on aircraft and spa...
A formalism is described for micromechanic impact of composites. The formalism consists of numerous ...
The need for accurate material models to simulate the deformation, damage and failure of polymer mat...
A general purpose orthotropic elasto-plastic computational constitutive material model has been deve...
A material model which incorporates several key capabilities which have been identified by the aeros...
A material model which incorporates several key capabilities which have been identified by the aeros...
The need for accurate material models to simulate the deformation, damage and failure of polymer mat...
An orthotropic elasto-plastic-damage three-dimensional model with tabulated input has been developed...
Dynamic tests were performed at NASA Langley Research Center on composite airframe structural compon...
A three-dimensional constitutive model has been developed for modeling orthotropic composites subjec...
Papers and working group summaries are presented which address composite material behavior and perfo...
An orthotropic three-dimensional material model suitable for use in modeling impact tests has been d...
A Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philoso...
FAA Technical Library2019PDFTech ReportUnited States. Department of Transportation. Federal Aviation...
A continuum damage model for the prediction of damage onset and structural collapse of structures ma...
This monograph is organized to look at: the successful application of composites on aircraft and spa...
A formalism is described for micromechanic impact of composites. The formalism consists of numerous ...
The need for accurate material models to simulate the deformation, damage and failure of polymer mat...
A general purpose orthotropic elasto-plastic computational constitutive material model has been deve...
A material model which incorporates several key capabilities which have been identified by the aeros...
A material model which incorporates several key capabilities which have been identified by the aeros...
The need for accurate material models to simulate the deformation, damage and failure of polymer mat...
An orthotropic elasto-plastic-damage three-dimensional model with tabulated input has been developed...
Dynamic tests were performed at NASA Langley Research Center on composite airframe structural compon...
A three-dimensional constitutive model has been developed for modeling orthotropic composites subjec...
Papers and working group summaries are presented which address composite material behavior and perfo...
An orthotropic three-dimensional material model suitable for use in modeling impact tests has been d...
A Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philoso...
FAA Technical Library2019PDFTech ReportUnited States. Department of Transportation. Federal Aviation...
A continuum damage model for the prediction of damage onset and structural collapse of structures ma...
This monograph is organized to look at: the successful application of composites on aircraft and spa...
A formalism is described for micromechanic impact of composites. The formalism consists of numerous ...