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Incorporation of Plasticity and Damage Into an Orthotropic Three-Dimensional Model with Tabulated Input Suitable for Use in Composite Impact ProblemsThe need for accurate material models to simulate the deformation, damage and failure of polymer matrix composites under impact conditions is becoming critical as these materials are gaining increased usage in the aerospace and automotive industries. While there are several composite material models currently available within commercial transient dynamic finite element codes, several features have been identified as being lacking in the currently available material models that could substantially enhance the predictive capability of the impact simulations. A specific desired feature pertains to the incorporation of both plasticity and damage within the material model. Another desired feature relates to using experimentally based tabulated stress-strain input to define the evolution of plasticity and damage as opposed to specifying discrete input properties (such as modulus and strength) and employing analytical functions to track the response of the material. To begin to address these needs, a combined plasticity and damage model suitable for use with both solid and shell elements is being developed for implementation within the commercial code LS-DYNA. The plasticity model is based on extending the Tsai-Wu composite failure model into a strain-hardening based orthotropic plasticity model with a non-associative flow rule. The evolution of the yield surface is determined based on tabulated stress-strain curves in the various normal and shear directions and is tracked using the effective plastic strain. The effective plastic strain is computed by using the non-associative flow rule in combination with appropriate numerical methods. To compute the evolution of damage, a strain equivalent semi-coupled formulation is used, in which a load in one direction results in a stiffness reduction in multiple coordinate directions. A specific laminated composite is examined to demonstrate the process of characterizing and analyzing the response of a composite using the developed model.
Document ID
20150019390
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Goldberg, Robert K.
(NASA Glenn Research Center Cleveland, OH United States)
Carney, Kelly S.
(NASA Glenn Research Center Cleveland, OH United States)
DuBois, Paul
(George Mason Univ. Fairfax, VA, United States)
Hoffarth, Canio
(Arizona State Univ. Tempe, AZ, United States)
Rajan, Subramaniam
(Arizona State Univ. Tempe, AZ, United States)
Blackenhorn, Gunther
(Livermore Software Technology Corp. CA, United States)
Date Acquired
October 14, 2015
Publication Date
August 1, 2015
Subject Category
Structural Mechanics
Composite Materials
Report/Patent Number
E-19123
NASA/TM-2015-218849
GRC-E-DAA-TN24915
Report Number: E-19123
Report Number: NASA/TM-2015-218849
Report Number: GRC-E-DAA-TN24915
Meeting Information
Meeting: American Society for Composites Annual Technical Conference
Location: East Lansing, MI
Country: United States
Start Date: September 28, 2015
End Date: September 30, 2015
Sponsors: American Society for Composites
Funding Number(s)
CONTRACT_GRANT: FAA 12-G-001
WBS: WBS 826611.04.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Impact
Finite Element Method
Polymer Matrix Composites
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