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Theoretical Development of an Orthotropic Elasto-Plastic Generalized Composite Material ModelThe need for accurate material models to simulate the deformation, damage and failure of polymer matrix composites 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 LS-DYNA (Registered), there are several features that have been identified that could improve the predictive capability of a composite model. To address these needs, a combined plasticity and damage model suitable for use with both solid and shell elements is being developed and is being implemented into LS-DYNA as MAT_213. A key feature of the improved material model is the use of tabulated stress-strain data in a variety of coordinate directions to fully define the stress-strain response of the material. To date, the model development efforts have focused on creating the plasticity portion of the model. The Tsai-Wu composite failure model has been generalized and extended to a strain-hardening based orthotropic material model with a non-associative flow rule. The coefficients of the yield function, and the stresses to be used in both the yield function and the flow rule, are computed based on the input stress-strain curves using the effective plastic strain as the tracking variable. The coefficients in the flow rule are computed based on the obtained stress-strain data. The developed material model is suitable for implementation within LS-DYNA for use in analyzing the nonlinear response of polymer composites.
Document ID
20150002335
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
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)
Harrington, Joseph
(Arizona State Univ. Tempe, AZ, United States)
Subramanian, Rajan
(Arizona State Univ. Tempe, AZ, United States)
Blankenhorn, Gunther
(Livermore Software Technology Corp. CA, United States)
Date Acquired
March 3, 2015
Publication Date
June 8, 2014
Subject Category
Structural Mechanics
Composite Materials
Report/Patent Number
GRC-E-DAA-TN14915
Meeting Information
Meeting: International LS-DYNA Users Conference
Location: Dearborn, MI
Country: United States
Start Date: June 8, 2014
End Date: June 10, 2014
Sponsors: Livermore Software Technology Corp.
Funding Number(s)
CONTRACT_GRANT: FAA-12-G-001
WBS: WBS 544163.04.01.03.01.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Plasticity
Finite Element Method
Polymer Matrix Composites
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