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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Serbian Society of Mechanics & Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade
2018-01-01
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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 |
work_keys_str_mv |
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