Constitutive modeling for FRP composite materials subject to extreme loading

A physically based, finite deformation, rate and temperature dependent theory and model have been developed to simulate the deformation and failure of FRP composite materials and structures. Failure modes include: inter alia, fiber crushing and kinking as occurs during extreme compressive loading; f...

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Main Authors: Asaro Robert J., Benson David
Format: Article
Language:English
Published: Serbian Society of Mechanics & Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade 2018-01-01
Series:Theoretical and Applied Mechanics
Subjects:
Online Access:http://www.doiserbia.nb.rs/img/doi/1450-5584/2018/1450-55841800011A.pdf
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spelling doaj-353bd62ad06049d784aba15bcb2a41612020-11-25T01:29:35ZengSerbian Society of Mechanics & Mathematical Institute of the Serbian Academy of Sciences and Arts, BelgradeTheoretical and Applied Mechanics1450-55842406-09252018-01-0145220523010.2298/TAM180415011A1450-55841800011AConstitutive modeling for FRP composite materials subject to extreme loadingAsaro Robert J.0Benson David1University of California, Department of Structural Engineering, San Diego, La Jolla, USAUniversity of California, Department of Structural Engineering, San Diego, La Jolla, USAA physically based, finite deformation, rate and temperature dependent theory and model have been developed to simulate the deformation and failure of FRP composite materials and structures. Failure modes include: inter alia, fiber crushing and kinking as occurs during extreme compressive loading; fiber fracture as occurs in for example fragmentation; interlaminar shear as occurs at elevated temperatures and that leads to kinking; debonding and delamination including the coupling with laminate kinking; and debonding as occurs in cored FRP panels. The theory/model is capable of describing quasi-static (including creep) as occurs at elevated temperatures, and dynamic deformation and failure as occurs during shock, blast or impact. The model is implemented within LS DYNA and specific example simulations are described that illustrate the theory/model capabilities. In Part I, fragmentation is not covered in detail. Fiber fracture and fragmentation are to be covered to detail with specific examples in Part II.http://www.doiserbia.nb.rs/img/doi/1450-5584/2018/1450-55841800011A.pdfFRP composite bucklingFRP composite compressive failure
collection DOAJ
language English
format Article
sources DOAJ
author Asaro Robert J.
Benson David
spellingShingle Asaro Robert J.
Benson David
Constitutive modeling for FRP composite materials subject to extreme loading
Theoretical and Applied Mechanics
FRP composite buckling
FRP composite compressive failure
author_facet Asaro Robert J.
Benson David
author_sort Asaro Robert J.
title Constitutive modeling for FRP composite materials subject to extreme loading
title_short Constitutive modeling for FRP composite materials subject to extreme loading
title_full Constitutive modeling for FRP composite materials subject to extreme loading
title_fullStr Constitutive modeling for FRP composite materials subject to extreme loading
title_full_unstemmed Constitutive modeling for FRP composite materials subject to extreme loading
title_sort constitutive modeling for frp composite materials subject to extreme loading
publisher Serbian Society of Mechanics & Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade
series Theoretical and Applied Mechanics
issn 1450-5584
2406-0925
publishDate 2018-01-01
description A physically based, finite deformation, rate and temperature dependent theory and model have been developed to simulate the deformation and failure of FRP composite materials and structures. Failure modes include: inter alia, fiber crushing and kinking as occurs during extreme compressive loading; fiber fracture as occurs in for example fragmentation; interlaminar shear as occurs at elevated temperatures and that leads to kinking; debonding and delamination including the coupling with laminate kinking; and debonding as occurs in cored FRP panels. The theory/model is capable of describing quasi-static (including creep) as occurs at elevated temperatures, and dynamic deformation and failure as occurs during shock, blast or impact. The model is implemented within LS DYNA and specific example simulations are described that illustrate the theory/model capabilities. In Part I, fragmentation is not covered in detail. Fiber fracture and fragmentation are to be covered to detail with specific examples in Part II.
topic FRP composite buckling
FRP composite compressive failure
url http://www.doiserbia.nb.rs/img/doi/1450-5584/2018/1450-55841800011A.pdf
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