Peridynamic modeling of thermo-oxidative damage evolution in a composite lamina

Selda Oterkus; Erdogan Madenci

Peridynamic modeling of thermo-oxidative damage evolution in a composite lamina

Selda Oterkus, Erdogan Madenci

Aerospace and Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

4 Scopus citations

Abstract

Surface oxidation degrades the durability of polymer matrix composites operating at high temperatures due to the presence of strong coupling between the thermal oxidation and structural damage evolution. The mechanism of oxidation in polymer matrix composites leads to shrinkage and damage growth. The thermo-oxidative behavior of composites introduces changes in diffusion behavior and mechanical response of the material. This study presents the derivation of peridynamic formulation for the thermo-oxidative behavior of the polymer matrix composites. As a demonstration, isothermal aging of a unidirectional composite lamina is considered by using peridynamics. It captures the effect of oxidation on damage growth and its propagation.

Original language	English (US)
Title of host publication	58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624104534
State	Published - 2017
Event	58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017 - Grapevine, United States Duration: Jan 9 2017 → Jan 13 2017

Other

Other	58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017
Country	United States
City	Grapevine
Period	1/9/17 → 1/13/17

ASJC Scopus subject areas

Mechanics of Materials
Architecture
Civil and Structural Engineering
Building and Construction

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Oterkus, S & Madenci, E 2017, Peridynamic modeling of thermo-oxidative damage evolution in a composite lamina. in 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, Grapevine, United States, 1/9/17.

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abstract = "Surface oxidation degrades the durability of polymer matrix composites operating at high temperatures due to the presence of strong coupling between the thermal oxidation and structural damage evolution. The mechanism of oxidation in polymer matrix composites leads to shrinkage and damage growth. The thermo-oxidative behavior of composites introduces changes in diffusion behavior and mechanical response of the material. This study presents the derivation of peridynamic formulation for the thermo-oxidative behavior of the polymer matrix composites. As a demonstration, isothermal aging of a unidirectional composite lamina is considered by using peridynamics. It captures the effect of oxidation on damage growth and its propagation.",

author = "Selda Oterkus and Erdogan Madenci",

year = "2017",

language = "English (US)",

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publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

note = "58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017 ; Conference date: 09-01-2017 Through 13-01-2017",

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AU - Oterkus, Selda

AU - Madenci, Erdogan

PY - 2017

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AB - Surface oxidation degrades the durability of polymer matrix composites operating at high temperatures due to the presence of strong coupling between the thermal oxidation and structural damage evolution. The mechanism of oxidation in polymer matrix composites leads to shrinkage and damage growth. The thermo-oxidative behavior of composites introduces changes in diffusion behavior and mechanical response of the material. This study presents the derivation of peridynamic formulation for the thermo-oxidative behavior of the polymer matrix composites. As a demonstration, isothermal aging of a unidirectional composite lamina is considered by using peridynamics. It captures the effect of oxidation on damage growth and its propagation.

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M3 - Conference contribution

AN - SCOPUS:85017389070

SN - 9781624104534

BT - 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017

Y2 - 9 January 2017 through 13 January 2017

ER -

Peridynamic modeling of thermo-oxidative damage evolution in a composite lamina

Abstract

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ASJC Scopus subject areas

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