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Publications (10 of 54) Show all publications
Olsson, R., Cameron, C., Moreau, F., Marklund, E., Merzkirch, M. & Pettersson, J. (2024). Design, Manufacture, and Cryogenic Testing of a Linerless Composite Tank for Liquid Hydrogen. Applied Composite Materials
Open this publication in new window or tab >>Design, Manufacture, and Cryogenic Testing of a Linerless Composite Tank for Liquid Hydrogen
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2024 (English)In: Applied Composite Materials, ISSN 0929-189X, E-ISSN 1573-4897Article in journal (Refereed) Epub ahead of print
Abstract [en]

This paper describes design, manufacture, and testing of a linerless composite vessel for liquid hydrogen, having 0.3 m diameter and 0.9 m length. The vessel consists of a composite cylinder manufactured by wet filament winding of thin-ply composite bands, bonded to titanium end caps produced by additive manufacturing. The aim was to demonstrate the linerless design concept with a thin-ply composite for the cylinder. The investigation is limited to the internal pressure vessel, while real cryogenic tanks also involve an outer vessel containing vacuum for thermal insulation. Thermal stresses dominate during normal operation (4 bar) and the layup was selected for equal hoop strains in the composite cylinder and end caps during filling with liquid hydrogen. Two vessels were tested in 20 cycles, by filling and emptying with liquid nitrogen to 4 bar, without signs of damage or leakage. Subsequently, one vessel was tested until burst at almost 30 bar.

Place, publisher, year, edition, pages
Springer Nature, 2024
Keywords
Cryogenic liquids; Cylinders (shapes); Elasticity; Hydrogen; Liquefied gases; Pressure vessels; Structural design; Tanks (containers); Thermal insulation; Burst tests; Composite cylinders; Composite tank; Composite vessels; Cryogenic testing; End caps; Linerless composite tanks; Liquid hydrogens; Ply composites; Thin ply; Filament winding
National Category
Mechanical Engineering
Identifiers
urn:nbn:se:ri:diva-72888 (URN)10.1007/s10443-024-10219-y (DOI)2-s2.0-85188127999 (Scopus ID)
Funder
Swedish Energy Agency, P2021-90268Swedish Energy Agency, P2021-90061
Note

Open access funding provided by RISE Research Institutes of Sweden. This work was to 92% funded by Energimyndigheten (the Swedish Energy Agency) through contract P2021-90061. Co-funding was provided by Oxeon AB. Finalisation of the manuscript has subsequently been funded by the internal development funds of RISE and Energimyndigheten (the Swedish Energy Agency) through contract P2021-90268 via the Competence Centre TechForH2

Available from: 2024-04-26 Created: 2024-04-26 Last updated: 2024-05-23Bibliographically approved
Sahbi Loukil, M., Costa, S., Bergwall, M., Deepthi Prasad, H. S., Moreau, F., Segersäll, M., . . . Olsson, R. (2024). Experimental and numerical investigation on bearing behavior of hybrid thin/thick-ply composite laminates. Composite structures, 331, Article ID 117888.
Open this publication in new window or tab >>Experimental and numerical investigation on bearing behavior of hybrid thin/thick-ply composite laminates
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2024 (English)In: Composite structures, ISSN 0263-8223, E-ISSN 1879-1085, Vol. 331, article id 117888Article in journal (Refereed) Published
Abstract [en]

Experimental and numerical studies were carried out to characterize hybrid thin- and thick-ply composite laminates and assess modelling capabilities. Five different composite laminates were manufactured using a single material system with varying proportions of thin plies (0%, 50%, and 100% thin-ply). Bearing tests were performed and the results from the tests were investigated. The results showed that performance, in terms of bearing strength at onset of damage and ultimate bearing stress, increased proportionally with the increasing amount of thin plies within the laminate. Microscopic examination of the failure modes for all laminates was performed at the center of the hole to determine the dominant failure mode. The numerical investigation uses a highly detailed mesoscale model previously validated for crash simulations but never used successfully to bearing damage areas. The results showed a good correlation regarding both the load response and the morphology of damage. 

Place, publisher, year, edition, pages
Elsevier Ltd, 2024
Keywords
Bearing strength, Composites, Hybrid laminate, Matrix crack, Thin Ply, Failure modes, Hybrid composites, Bearing behaviors, Bearing strengths, Composite laminate, Experimental and numerical studies, Experimental investigations, Hybrid laminates, Numerical investigations, Ply composites, Laminated composites
National Category
Materials Engineering
Identifiers
urn:nbn:se:ri:diva-71952 (URN)10.1016/j.compstruct.2024.117888 (DOI)2-s2.0-85182392642 (Scopus ID)
Available from: 2024-02-27 Created: 2024-02-27 Last updated: 2024-05-22Bibliographically approved
Singh, V., Larsson, R., Olsson, R. & Marklund, E. (2024). Rate dependent compressive failure and delamination growth in multidirectional composite laminates. Journal of composite materials, 58(3), 419
Open this publication in new window or tab >>Rate dependent compressive failure and delamination growth in multidirectional composite laminates
2024 (English)In: Journal of composite materials, ISSN 0021-9983, E-ISSN 1530-793X, Vol. 58, no 3, p. 419-Article, review/survey (Refereed) Published
Abstract [en]

A novel intralaminar model has, for the first time, been applied and validated for the rate-dependent failure of multidirectional carbon/epoxy laminates. Quasi-static compressive failure is evaluated by the growth of intralaminar rate-dependent damage combined with the interaction of cohesive zones for interlaminar delamination. A special feature of the intralaminar model is the homogenised ply response, allowing simultaneous damage-degradation of the polymer matrix combined with the fibres. To model the observed quasi-brittle failure response of the plies under finite deformation, we have used a viscoelastic-viscoplastic matrix combined with damage and isotropic hardening behaviour. Elastic transverse isotropy is used to model the fibre reinforcement of the plies. Standard cohesive surfaces are used to model the initiation and propagation of delamination. Numerical simulations using ABAQUS/Explicit are performed to predict the growth and delamination of intralaminar damage under compression in different laminates with 56 plies of IM7/8552 carbon/epoxy. Predictions of stress versus strain and damage growth are shown to agree well with experimental results for a range of strain rates and stacking sequences. 

Place, publisher, year, edition, pages
SAGE Publications Ltd, 2024
Keywords
Brittle fracture; Carbon; Ductile fracture; Hardening; Laminated composites; Strain rate; Viscoplasticity; Angle ply laminate; Cohesive surface; Composite laminate; Compressive failure; Continuum damage; Delamination growth; Dependent failure; Isotropic hardenings; Rate dependent; Viscoelasticity-viscoplasticity; Viscoelasticity
National Category
Composite Science and Engineering
Identifiers
urn:nbn:se:ri:diva-68794 (URN)10.1177/00219983231215688 (DOI)2-s2.0-85178417981 (Scopus ID)
Funder
Swedish Foundation for Strategic Research, FID16-0041
Note

The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was supported by the Swedish Foundation for Strategic Research (SSF) through the contract dnr FID16-0041 and by the internal SK-development funds of RISE.

Available from: 2024-01-10 Created: 2024-01-10 Last updated: 2024-05-27Bibliographically approved
Singh, V., Larsson, R., Olsson, R. & Marklund, E. (2023). A micromechanics based model for rate dependent compression loaded unidirectional composites. Composites Science And Technology, 232, Article ID 109821.
Open this publication in new window or tab >>A micromechanics based model for rate dependent compression loaded unidirectional composites
2023 (English)In: Composites Science And Technology, ISSN 0266-3538, E-ISSN 1879-1050, Vol. 232, article id 109821Article in journal (Refereed) Published
Abstract [en]

Strain-rate effects in a unidirectional non-crimp fabric carbon/epoxy composite are addressed. To allow for kink-band formation including strain-rate effects and damage in such composites, the paper advances a recent model focused on compression loading at small off-axis angles. The model is based on computational homogenization with a subscale represented by matrix and fibre constituents at finite deformation. The fibre constituent is assumed to be elastic transversely isotropic and the matrix is viscoelastic–viscoplastic with damage degradation. Novel model improvements of special importance to small off-axis loading relate to the isostress formulation of the homogenized response in transverse shear. In this context, an enhanced homogenized elastic response is proposed based on Halpin–Tsai corrections to account for the nonuniform stress distribution on the microscale. The model captures the strongly rate sensitive kink-band formation due to localized matrix shearing and fibre rotation, confirming the experimentally observed increase in compressive strength for high strain rates. © 2022 The Author(s)

Place, publisher, year, edition, pages
Elsevier Ltd, 2023
Keywords
A. Structural composites, B. Non-linear behaviour, C. Damage mechanics, C. Material modelling, Viscoelasticity–viscoplasticity, Compressive strength, Strain rate, A structural composite, B non-linear behavior, C damage mechanic, C material modeling, Damage-mechanics, Material modeling, matrix, Nonlinear behaviours, Structural composites, Viscoelasticity
National Category
Applied Mechanics
Identifiers
urn:nbn:se:ri:diva-61350 (URN)10.1016/j.compscitech.2022.109821 (DOI)2-s2.0-85142492701 (Scopus ID)
Note

 Funding details: University of Patras; Funding details: H2020 Marie Skłodowska-Curie Actions, MSCA, 721256; Funding details: Stiftelsen för Strategisk Forskning, SSF, FID16-0041, P113521, SK-projects P108811; Funding text 1: The model development was funded by the Swedish Foundation for Strategic Research (SSF, dnr FID16-0041), with co-funding from RISE internal development funds, Sweden (SK-projects P108811 and P113521). The experiments were funded by the ICONIC project under the Marie Skłodowska-Curie, Sweden grant No 721256. G. Lampeas and B. Ravindran at University of Patras are acknowledged for assistance with experimental data, which allowed us to validate our model.; Funding text 2: The model development was funded by the Swedish Foundation for Strategic Research ( SSF, dnr FID16-0041 ), with co-funding from RISE internal development funds, Sweden (SK-projects P108811 and P113521). The experiments were funded by the ICONIC project under the Marie Skłodowska-Curie, Sweden grant No 721256 . G. Lampeas and B. Ravindran at University of Patras are acknowledged for assistance with experimental data, which allowed us to validate our model.

Available from: 2022-12-09 Created: 2022-12-09 Last updated: 2023-06-07Bibliographically approved
Larsson, R., Singh, V., Olsson, R. & Marklund, E. (2022). A micromechanically based model for dynamic damage evolution in unidirectional composites. International Journal of Solids and Structures, 238, Article ID 111368.
Open this publication in new window or tab >>A micromechanically based model for dynamic damage evolution in unidirectional composites
2022 (English)In: International Journal of Solids and Structures, ISSN 0020-7683, E-ISSN 1879-2146, Vol. 238, article id 111368Article in journal (Refereed) Published
Abstract [en]

This article addresses the micromechanically motivated, quasistatic to dynamic, failure response of fibre reinforced unidirectional composites at finite deformation. The model draws from computational homogenization, with a subscale represented by matrix and fibre constituents. Undamaged matrix response assumes isotropic viscoelasticity–viscoplasticity, whereas the fibre is transversely isotropic hyperelastic. Major novelties involve damage degradation of the matrix response, due to shear in compression based on a rate dependent damage evolution model, and the large deformation homogenization approach. The homogenized quasi-brittle damage induced failure is described by elastically stored isochoric energy and plastic work of the undamaged polymer, driving the evolution of damage. The developed model is implemented in ABAQUS/Explicit. Finite element validation is carried out for a set of off-axis experimental compression tests in the literature. Considering the unidirectional carbon–epoxy (IM7/8552) composite at different strain rates, it appears that the homogenized damage degraded response can represent the expected ductile failure of the composite at compressive loading with different off-axes. Favourable comparisons are made for the strain and fibre rotation distribution involving localized shear and fibre kinking. © 2021 The Authors

Place, publisher, year, edition, pages
Elsevier Ltd, 2022
Keywords
Continuum damage, Homogenization, Off-axis compression loading, Unidirectional ply, Viscoplasticity, ABAQUS, Compression testing, Deformation, Plasticity, Strain rate, Compression loading, Damage evolution, Dynamic damage, matrix, Off-axis, Unidirectional composites, Fibers
National Category
Composite Science and Engineering
Identifiers
urn:nbn:se:ri:diva-57498 (URN)10.1016/j.ijsolstr.2021.111368 (DOI)2-s2.0-85121235543 (Scopus ID)
Note

Funding details: 721256; Funding details: Stiftelsen för Strategisk Forskning, SSF, 25201, FID16-0041; Funding details: VINNOVA, 2016-04239; Funding details: Horizon 2020; Funding text 1: The authors gratefully acknowledge the support of the ICONIC project under the Marie Skłodowska-Curie grant agreement No 721256 of the European Union Horizon 2020 research and innovation programme . Co-funding has also been provided from the Swedish FFI programme via VINNOVA (dnr 2016-04239 ), SSF, Sweden (dnr FID16-0041 ) and from the development funds of RISE, Sweden (RISE SICOMP SK-project 25201).

Available from: 2021-12-30 Created: 2021-12-30 Last updated: 2023-06-07Bibliographically approved
Costa, S., Zrida, H., Olsson, R., Herráez, M. & Östlund, R. (2022). A unified physically-based finite deformation model for damage growth in composites. Composites. Part A, Applied science and manufacturing, 161, Article ID 107103.
Open this publication in new window or tab >>A unified physically-based finite deformation model for damage growth in composites
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2022 (English)In: Composites. Part A, Applied science and manufacturing, ISSN 1359-835X, E-ISSN 1878-5840, Vol. 161, article id 107103Article in journal (Refereed) Published
Abstract [en]

Two 3D homogenized models for damage growth in a unidirectional (UD) composite ply are simplified and merged into a unified model. The fibre kinking behaviour is based on fibre kinking theory handled in a finite deformation framework. The nonlinear shear behaviour is pressure dependent and is modelled by combining damage and friction on the fracture plane. Fibre kinking growth and transverse behaviour are modelled with a single damage variable. This allows both modes to occur simultaneously and mutually influence each other in an efficient and physically-based way. For validation the model is tested against micro-mechanical Finite Element (FE) simulations under pure longitudinal compression and influenced by shear. The results show nearly perfect agreement for stiffness, strength and crushing stress. The model validation is performed against two different components under three-point bending and a quasi-static crash scenario. Both simulation show good correlation with experiments, validating thus the present unified model. © 2022 The Author(s)

Place, publisher, year, edition, pages
Elsevier Ltd, 2022
Keywords
Continuum damage modelling, Crash, Fibre kinking, Continuum damage mechanics, Fibers, Continuum damage model, Damage growth, Deformation modeling, Fiber-kinking, Finite deformations, Homogenized model, Physically based, Unidirectional composites, Unified Modeling, Deformation
National Category
Mechanical Engineering
Identifiers
urn:nbn:se:ri:diva-60052 (URN)10.1016/j.compositesa.2022.107103 (DOI)2-s2.0-85135300033 (Scopus ID)
Note

Funding details: 2016-04239; Funding details: Energimyndigheten, 50179-1; Funding text 1: This work was funded by Energimyndigheten (Swedish Energy Agency) , project number 50179-1 ; and co-funded by Gestamp Hardtech . The authors are also grateful for access to complementary material data from Volvo Cars and experimental data for the crash tube from Volvo Trucks, obtained within the project “FFI-Crash 2” (Dnr 2016-04239), jointly funded by the industry and the Swedish Innovation Agency Vinnova .

Available from: 2022-09-05 Created: 2022-09-05 Last updated: 2023-06-07Bibliographically approved
McElroy, M., André, A., Goode, T., Costa, S., Olsson, R. & Pankow, M. (2021). Use of enriched shell elements compared to solid elements for modelling delamination growth during impact on composites. Composite structures, 269, Article ID 113945.
Open this publication in new window or tab >>Use of enriched shell elements compared to solid elements for modelling delamination growth during impact on composites
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2021 (English)In: Composite structures, ISSN 0263-8223, E-ISSN 1879-1085, Vol. 269, article id 113945Article in journal (Refereed) Published
Abstract [en]

Simulation of damage in composite laminates using currently available three-dimensional finite element tools is computationally demanding often to the point that analysis is not practical. This paper presents an enriched shell element that can provide a computationally efficient means to simulate low-velocity impact damage in a composite. The enriched element uses the Floating Node Method and a damage algorithm based on the Virtual Crack Closure Technique that is capable of simulating progressive damage growth consisting of delamination and delamination-migrations from ply to ply during a dynamic impact load. This paper presents results from the shell model in a test-analysis correlation for impact testing of 7-ply and 56-ply laminates. Analysis results from a separate high-fidelity three-dimensional finite element analysis are included also for comparison in the case of the 7-ply laminate, but not in the case the 56-ply laminate due to excessive computational demand. This paper serves as the first application of both models in low-velocity impact simulation. The shell model is considerably more computationally efficient than the high-fidelity model by at least an order of magnitude and is shown to produce results, while not as accurate as the high-fidelity model, potentially sufficiently accurate for a wide range of engineering applications including structural design and rapid prototype assessments.

Place, publisher, year, edition, pages
Elsevier Ltd, 2021
Keywords
Delamination, Laminates, Low-velocity impact, Mechanical testing, Computational efficiency, Crack closure, Finite element method, Impact testing, Shells (structures), Composite laminate, Computationally efficient, Delamination growth, High fidelity models, Low velocity impact, Mechanical, Ply laminates, Shell element, Shell models, Solid elements
National Category
Composite Science and Engineering
Identifiers
urn:nbn:se:ri:diva-53009 (URN)10.1016/j.compstruct.2021.113945 (DOI)2-s2.0-85105359536 (Scopus ID)
Note

Funding details: National Science Foundation, NSF, DGE-1746939; Funding details: Langley Research Center, LaRC; Funding text 1: This research is based in part upon work supported by the National Science Foundation Graduate Research Fellowship Program under Grant No. DGE-1746939. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the authors and do not necessarily reflect the views of the National Science Foundation. The research was also funded in part by NASA Langley Research Center and RISE SICOMP. The authors would like to thank Dr. T. Kevin O’Brien for his advice and consultation. The simulation work performed by Rodrigo Machado is gratefully appreciated.

Available from: 2021-05-26 Created: 2021-05-26 Last updated: 2023-06-07Bibliographically approved
Larsson, R., Singh, V., Olsson, R. & Marklund, E. (2020). A micromechanically based model for strain rate effects in unidirectional composites. Mechanics of materials, 148, Article ID 103491.
Open this publication in new window or tab >>A micromechanically based model for strain rate effects in unidirectional composites
2020 (English)In: Mechanics of materials, ISSN 0167-6636, E-ISSN 1872-7743, Vol. 148, article id 103491Article in journal (Refereed) Published
Abstract [en]

This article addresses dynamic behaviour of fibre reinforced polymer composites in terms of a transversely isotropic viscoelastic-viscoplastic constitutive model established at the unidirectional ply level. The model captures the prelocalized response of the ply in terms of rate dependent elasticity and strength without damage. A major novelty is that the model draws from computational homogenization, with matrix and fibre materials as subscale constituents for a representative volume element of the ply. The micromechanics of the strain rate dependent polymer matrix is represented by an isotropic pressure sensitive viscoelastic-viscoplastic prototype model. For the fibre material, transverse elasticity is assumed. The constituents are homogenized via the fluctuating strain of the subscale, where a simple ansatz is applied to allow for constant stress in the plane transverse to the fibre orientation. Despite the relatively simple modelling assumptions for the constituents, the homogenized model compares favourably to experimental data for an epoxy/carbon fibre based composite, subjected to a variety of challenging uniaxial off-axis tests. The model response clearly reflects observed strain rate dependencies under both tensile and compressive loadings. 

Place, publisher, year, edition, pages
Elsevier B.V., 2020
Keywords
Micromechanics, Off-axis loading, Strain rate dependence, Unidirectional (UD) ply, Elasticity, Fiber reinforced plastics, Fibers, Viscoelasticity, Computational homogenization, Fibre-reinforced polymer composites, Representative volume element (RVE), Strain rate dependency, Tensile and compressive loading, Transversely isotropic, Unidirectional composites, Viscoplastic constitutive modeling, Strain rate
National Category
Natural Sciences
Identifiers
urn:nbn:se:ri:diva-45150 (URN)10.1016/j.mechmat.2020.103491 (DOI)2-s2.0-85086576741 (Scopus ID)
Note

Funding details: Horizon 2020 Framework Programme, H2020; Funding details: H2020 Marie Skłodowska-Curie Actions, MSCA, 721256; Funding details: VINNOVA, 25173-1, 2016-04239; Funding text 1: The authors gratefully acknowledge the support of the ICONIC project under the Marie Skłodowska-Curie grant agreement No 721256 of the European Union Horizon 2020 research and innovation programme. Co-funding has also been provided from the Swedish FFI programme via VINNOVA (dnr 2016-04239) and from the development funds of RISE ( RISE SICOMP SK-project 25173-1).

Available from: 2020-07-13 Created: 2020-07-13 Last updated: 2024-01-17Bibliographically approved
Costa, S., Fagerström, M. & Olsson, R. (2020). Development and validation of a finite deformation fibre kinking model for crushing of composites. Composites Science And Technology, 197, Article ID 108236.
Open this publication in new window or tab >>Development and validation of a finite deformation fibre kinking model for crushing of composites
2020 (English)In: Composites Science And Technology, ISSN 0266-3538, E-ISSN 1879-1050, Vol. 197, article id 108236Article in journal (Refereed) Published
Abstract [en]

A mesoscale model for fibre kinking onset and growth in a three-dimensional framework is developed and validated against experimental results obtained in-house as well as from the literature. The model formulation is based on fibre kinking theory i.e. the initially misaligned fibres rotate due to compressive loading and nonlinear shear behaviour. Furthermore, the physically-based response is computed in a novel and efficient way using finite deformation theory. The model validation starts by correlating the numerical results against compression tests of specimens with a known misalignment. The results show good agreement of stiffness and strength for two specimens with low and high misalignment. Fibre kinking growth is validated by simulating the crushing of a flat coupon with the fibres oriented to the load direction. The numerical results show very good agreement with experiments in terms of crash morphology and load response.

National Category
Engineering and Technology
Identifiers
urn:nbn:se:ri:diva-45049 (URN)10.1016/j.compscitech.2020.108236 (DOI)2-s2.0-85085275478 (Scopus ID)
Available from: 2020-06-02 Created: 2020-06-02 Last updated: 2023-06-07Bibliographically approved
Singh, V., Larsson, R., Marklund, E. & Olsson, R. (2019). Effect of strain rate at compressive and tensile loading of unidirectional plies in structural composites. In: Turon A, Maimí P, Fagerström M (Ed.), Proc. 7th ECCOMAS Thematic Conf. on the Mechanical Response of Composites.: . Paper presented at 7th ECCOMAS Thematic Conf. on the Mechanical Response of Composites. (pp. 177-183). European Community on Computational Methods in Applied Science (ECCOMAS)
Open this publication in new window or tab >>Effect of strain rate at compressive and tensile loading of unidirectional plies in structural composites
2019 (English)In: Proc. 7th ECCOMAS Thematic Conf. on the Mechanical Response of Composites. / [ed] Turon A, Maimí P, Fagerström M, European Community on Computational Methods in Applied Science (ECCOMAS) , 2019, p. 177-183Conference paper, Published paper (Other academic)
Abstract [en]

Fibre-reinforced polymer composites are widely used in structural applications due to their high specific stiffness and strength. In some applications the response of dynamically loaded composite components must be analysed. For example, in crash analyses of structural components, where very high loading rates occurs, the composite behaviour is not fully understood. For this, we present a novel transversely isotropic viscoelasticviscoplastic constitutive model for a unidirectional carbon-epoxy composite. The model is micromechanically motivated so that the matrix and fibre materials of the composite are treated as micromechanical constituents at the ply scale. Based on the Hill-Mandel condition, the phases are homogenized via the macroscopic and fluctuating strain fields. To arrive at a simple but still representative model, a simplistic ansatz is applied to the structure of the fluctuating strains leading to a non-standard homogenized response of the composite. The model is applied to the non-linear rate dependent anisotropic ply behaviour under quasi-static and dynamic loading at different off-axis angles. For a simple viscoelastic-viscoplastic prototype for the rate dependent matrix response, there is a good correlation between measured and model response of the IM7-8552 material system in compression and tension.

Place, publisher, year, edition, pages
European Community on Computational Methods in Applied Science (ECCOMAS), 2019
Keywords
Constitutive model, Strain rate effects, Unidirectional composites
National Category
Applied Mechanics
Identifiers
urn:nbn:se:ri:diva-42513 (URN)
Conference
7th ECCOMAS Thematic Conf. on the Mechanical Response of Composites.
Projects
ICONICFFI-Crash 2
Funder
EU, Horizon 2020, Grant 721256Vinnova, Dnr 2016-04239
Available from: 2020-01-09 Created: 2020-01-09 Last updated: 2023-06-07Bibliographically approved
Organisations
Identifiers
ORCID iD: ORCID iD iconorcid.org/0000-0002-2627-3280

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