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    Rights statement: This is the author’s version of a work that was accepted for publication in Composite Strutures. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published in Composite Structures, 282, 2022 DOI: 10.1016/j.compstruct.2021.115107

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Design optimisation of braided composite beams for lightweight rail structures using machine learning methods

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Design optimisation of braided composite beams for lightweight rail structures using machine learning methods. / Singh, A.; Gu, Z.; Hou, X. et al.
In: Composite Structures, Vol. 282, 115107, 15.02.2022.

Research output: Contribution to Journal/MagazineJournal articlepeer-review

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Singh A, Gu Z, Hou X, Liu Y, Hughes DJ. Design optimisation of braided composite beams for lightweight rail structures using machine learning methods. Composite Structures. 2022 Feb 15;282:115107. Epub 2021 Dec 14. doi: 10.1016/j.compstruct.2021.115107

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Bibtex

@article{8960e109db434ee0868430893088bc1f,
title = "Design optimisation of braided composite beams for lightweight rail structures using machine learning methods",
abstract = "Braided composites have seen substantial industrial uptake for structural applications in the past decade. The dependence of their properties on braid angle provides opportunities for lightweighting through structure-specific optimisation. This paper presents an integrated approach, combining finite element (FE) simulations and a genetic algorithm (GA) to optimise braided beam structures in the spaceframe chassis of a rail vehicle. The braid angle and number of layers for each beam were considered as design variables. A set of 200 combinations of these variables were identified using a sampling strategy for FE simulations. The results were utilised to develop a surrogate model using genetic programming (GP) to correlate the design variables with structural mass and FE-predicted chassis displacements under standard loads. The surrogate model was then used to optimise the design variables using GA to minimise mass without compromising mechanical performance. The optimised design rendered approximately 15.7% weight saving compared to benchmark design. ",
keywords = "Braided composites, Design optimisation, Finite element analysis, Genetic algorithm, Genetic programming, Lightweighting, Benchmarking, Chassis, Composite materials, Finite element method, Machine learning, Structural optimization, Composite beam, Design optimization, Design variables, Finite element analyse, Finite elements simulation, Machine learning methods, Structural applications, Surrogate modeling, Genetic algorithms",
author = "A. Singh and Z. Gu and X. Hou and Y. Liu and D.J. Hughes",
note = "This is the author{\textquoteright}s version of a work that was accepted for publication in Composite Strutures. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published in Composite Structures, 282, 2022 DOI: 10.1016/j.compstruct.2021.115107 ",
year = "2022",
month = feb,
day = "15",
doi = "10.1016/j.compstruct.2021.115107",
language = "English",
volume = "282",
journal = "Composite Structures",
issn = "0263-8223",
publisher = "Elsevier Ltd",

}

RIS

TY - JOUR

T1 - Design optimisation of braided composite beams for lightweight rail structures using machine learning methods

AU - Singh, A.

AU - Gu, Z.

AU - Hou, X.

AU - Liu, Y.

AU - Hughes, D.J.

N1 - This is the author’s version of a work that was accepted for publication in Composite Strutures. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published in Composite Structures, 282, 2022 DOI: 10.1016/j.compstruct.2021.115107

PY - 2022/2/15

Y1 - 2022/2/15

N2 - Braided composites have seen substantial industrial uptake for structural applications in the past decade. The dependence of their properties on braid angle provides opportunities for lightweighting through structure-specific optimisation. This paper presents an integrated approach, combining finite element (FE) simulations and a genetic algorithm (GA) to optimise braided beam structures in the spaceframe chassis of a rail vehicle. The braid angle and number of layers for each beam were considered as design variables. A set of 200 combinations of these variables were identified using a sampling strategy for FE simulations. The results were utilised to develop a surrogate model using genetic programming (GP) to correlate the design variables with structural mass and FE-predicted chassis displacements under standard loads. The surrogate model was then used to optimise the design variables using GA to minimise mass without compromising mechanical performance. The optimised design rendered approximately 15.7% weight saving compared to benchmark design.

AB - Braided composites have seen substantial industrial uptake for structural applications in the past decade. The dependence of their properties on braid angle provides opportunities for lightweighting through structure-specific optimisation. This paper presents an integrated approach, combining finite element (FE) simulations and a genetic algorithm (GA) to optimise braided beam structures in the spaceframe chassis of a rail vehicle. The braid angle and number of layers for each beam were considered as design variables. A set of 200 combinations of these variables were identified using a sampling strategy for FE simulations. The results were utilised to develop a surrogate model using genetic programming (GP) to correlate the design variables with structural mass and FE-predicted chassis displacements under standard loads. The surrogate model was then used to optimise the design variables using GA to minimise mass without compromising mechanical performance. The optimised design rendered approximately 15.7% weight saving compared to benchmark design.

KW - Braided composites

KW - Design optimisation

KW - Finite element analysis

KW - Genetic algorithm

KW - Genetic programming

KW - Lightweighting

KW - Benchmarking

KW - Chassis

KW - Composite materials

KW - Finite element method

KW - Machine learning

KW - Structural optimization

KW - Composite beam

KW - Design optimization

KW - Design variables

KW - Finite element analyse

KW - Finite elements simulation

KW - Machine learning methods

KW - Structural applications

KW - Surrogate modeling

KW - Genetic algorithms

U2 - 10.1016/j.compstruct.2021.115107

DO - 10.1016/j.compstruct.2021.115107

M3 - Journal article

VL - 282

JO - Composite Structures

JF - Composite Structures

SN - 0263-8223

M1 - 115107

ER -