NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Multiscale Modeling of Thermoplastics Using Atomistic-informed MicromechanicsA multiscale model was developed for predicting the thermoelastic behavior of semi-crystalline thermoplastic materials for composite aerospace applications. At the highest scale containing the semi-crystalline spherulite in an amorphous matrix, the generalized method of cells, or high fidelity method of cells, was used to perform the homogenization calculations to obtain the effective properties. Models were developed assuming a cubic, or spherical shape, for the spherulite to understand if the morphology of the spherulite affects the effective thermoelastic properties. The generalized method of cells was used to model at the repeating unit cells at the subscales of the microstructure including the lamellae stacks and granular crystal blocks. The scales are integrated using the multiscale micromechanics method in the NASA Multiscale Analysis Tool. Data from molecular dynamics simulations were used as inputs for the amorphous and crystalline constituents. Convergence studies were performed to determine the best level of discretization for the repeating unit cell at the highest scale. Effective Young’s modulus, shear modulus, Poisson’s ratio, coefficient of thermal expansion, and thermal conductivity were predicted for polyether ether ketone and polyether ketone ketone, and very good agreement between the model utilizing the cubic spherulite and the experimental data, where available, was observed for polyether ketone ketone. Normalization of the data for the bulk polyether ketone ketone, against amorphous data, improved the predictions as compared to experimental data. Overall, the high fidelity method of cells
predicted a stiffer response then the generalized method of cells as the crystallinity was increased. The shape of the spherulite had a minimal effect on the predicted bulk properties of the polymers.
Document ID
20220019197
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Evan J. Pineda
(Glenn Research Center Cleveland, Ohio, United States)
Jamal F. Husseini
(University of Massachusetts Lowell Lowell, Massachusetts, United States)
Joshua D. Kemppainen
(Michigan Technological University Houghton, Michigan, United States)
Brett A. Bednarcyk
(Glenn Research Center Cleveland, Ohio, United States)
William A. Pisani
(U.S Army Engineer Research and Development Center)
Gregory M. Odegard
(Michigan Technological University Houghton, Michigan, United States)
Scott E. Stapleton
(University of Massachusetts Lowell)
Date Acquired
December 22, 2022
Subject Category
Chemistry and Materials (General)
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 966826.02.03.1655.23
INTERAGENCY: SAA3-1697
WBS: 264925.04.27.22
CONTRACT_GRANT: 80NSSC21K1285
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
thermoplastics
multiscale modeling
molecular dynamics
micromechanics
NASMAT
PEEK
PEKK
Elastic Properties
Coefficient of thermal expansion
thermal conductivity
generalized method of cells
high fidelity generalized method of cells
vector based constitutive laws
multiscale recursive micromechanics
No Preview Available