Three-dimensional constitutive relations of aligned carbon nanotube polymer nanocomposites

D. Handlin, R. Guzmán de Villoria, S. H. Chan, H. Cebeci, M. Williams, E. M. Parsons, S. Socrate, B. L. Wardle, S. Scotti, J. Kim

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

4 Citations (Scopus)

Abstract

High volume fraction aligned carbon nanotube (CNT) polymer nanocomposites (A-PNCs) are fabricated by biaxial mechanical densification of the CNTs, followed by polymer infiltration via capillarity-assisted wetting using an aerospace-grade epoxy. These A-PNCs are then tested in tension in order to determine the full constitutive relation of the material. Prior to this work, only bulk compression or nanomechanical tests have been attempted due to the small size of the samples. Elastic stiffness derived from optical strain mapping is in agreement both with prior experimental nanoindentation measurements and finite element calculations that include the effects of waviness of the reinforcing CNT 'fibers'. Results from longitudinal and transverse testing are shown for 0, 4, and 6 % volume fraction CNT reinforcement, and imaging via scanning electron microscopy and micro-computed tomography is used to establish morphology. Future work includes tests to establish the shear modulus and complete the full constitutive relation as a function of CNT volume fraction.

Original languageEnglish
Title of host publication54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
DOIs
Publication statusPublished - 2013
Externally publishedYes
Event54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Boston, MA, United States
Duration: 8 Apr 201311 Apr 2013

Publication series

Name54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Conference

Conference54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Country/TerritoryUnited States
CityBoston, MA
Period8/04/1311/04/13

Funding

This work was supported by Boeing, EADS, Embraer, Lockheed Martin, Saab AB, Composite Systems Technology, Hexcel, and TohoTenax through MIT’s Nano-Engineered Composite aerospace STructures (NECST) Consortium and in part by the U.S. Army Research Office under contract W911NF-07-D-0004 and W911NF-13-D-0001. Daniel Handlin’s work is supported by NASA Space Technology Research Fellowship Grant #NNX11AN79H. The authors thank Sunny Wicks (MIT), Richard Li (MIT), John Kane (MIT) and the entire necstlab at MIT for technical support and advice. This work made use of the Shared Experimental Facilities supported in part by the MRSEC Program of the National Science Foundation under award number DMR-0819762 and was carried out in part through the use of MIT’s Microsystems Technology Laboratories.

FundersFunder number
TohoTenax
National Science FoundationDMR-0819762
Boeing
National Aeronautics and Space Administration11AN79H
Army Research OfficeW911NF-13-D-0001, W911NF-07-D-0004

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