Graphene in aerospace composites: characterising thermal response

Asimina Manta; Matthieu Gresil; Constantinos Soutis

doi:10.1063/1.5024145

Graphene in aerospace composites: characterising thermal response

Asimina Manta, Matthieu Gresil, Constantinos Soutis

Research output: Chapter in Book/Report/Conference proceeding › Conference Paper › Other

11 Citations (Scopus)

Abstract

In this work, a numerical model is presented to describe the thermal response of a graphene/polymer nanocomposite. The approach is based on the multi-scale method and consists of a unit cell and a Representative Volume Element (RVE) built on a finite element interface. At the unit cell level, the material's nano-characteristics (filler geometry, phase thermal properties, interfacial properties) are employed to calculate the local thermal conductivity. The material's architecture is modelled at the RVE level by incorporating the previously obtained local thermal properties. A statistical sample was studied and the average thermal response was compared to experimental data.

Original language	English
Title of host publication	AIP Conference Proceedings
Number of pages	9
DOIs	https://doi.org/10.1063/1.5024145
Publication status	Published - 21 Feb 2018
Externally published	Yes
Event	International Conference on Structural Analysis of Advanced Materials 2017 - Bucharest, Romania Duration: 19 Sept 2017 → 22 Sept 2017 Conference number: 7th http://www.icsaam2017.pub.ro/

Conference

Conference	International Conference on Structural Analysis of Advanced Materials 2017
Abbreviated title	ICSAAM 2017
Country/Territory	Romania
City	Bucharest
Period	19/09/17 → 22/09/17
Internet address	http://www.icsaam2017.pub.ro/

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10.1063/1.5024145

Cite this

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title = "Graphene in aerospace composites: characterising thermal response",

abstract = "In this work, a numerical model is presented to describe the thermal response of a graphene/polymer nanocomposite. The approach is based on the multi-scale method and consists of a unit cell and a Representative Volume Element (RVE) built on a finite element interface. At the unit cell level, the material's nano-characteristics (filler geometry, phase thermal properties, interfacial properties) are employed to calculate the local thermal conductivity. The material's architecture is modelled at the RVE level by incorporating the previously obtained local thermal properties. A statistical sample was studied and the average thermal response was compared to experimental data.",

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T1 - Graphene in aerospace composites

T2 - International Conference on Structural Analysis of Advanced Materials 2017

AU - Manta, Asimina

AU - Gresil, Matthieu

AU - Soutis, Constantinos

N1 - Conference code: 7th

PY - 2018/2/21

Y1 - 2018/2/21

N2 - In this work, a numerical model is presented to describe the thermal response of a graphene/polymer nanocomposite. The approach is based on the multi-scale method and consists of a unit cell and a Representative Volume Element (RVE) built on a finite element interface. At the unit cell level, the material's nano-characteristics (filler geometry, phase thermal properties, interfacial properties) are employed to calculate the local thermal conductivity. The material's architecture is modelled at the RVE level by incorporating the previously obtained local thermal properties. A statistical sample was studied and the average thermal response was compared to experimental data.

AB - In this work, a numerical model is presented to describe the thermal response of a graphene/polymer nanocomposite. The approach is based on the multi-scale method and consists of a unit cell and a Representative Volume Element (RVE) built on a finite element interface. At the unit cell level, the material's nano-characteristics (filler geometry, phase thermal properties, interfacial properties) are employed to calculate the local thermal conductivity. The material's architecture is modelled at the RVE level by incorporating the previously obtained local thermal properties. A statistical sample was studied and the average thermal response was compared to experimental data.

UR - https://www.scopus.com/pages/publications/85042926188

U2 - 10.1063/1.5024145

DO - 10.1063/1.5024145

M3 - Conference Paper

AN - SCOPUS:85042926188

BT - AIP Conference Proceedings

Y2 - 19 September 2017 through 22 September 2017

ER -

Graphene in aerospace composites: characterising thermal response

Abstract

Conference

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