Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm

This work investigates thermal aeroelastic tailoring of a laminated composite panel with a lamination parameter-based method. Equivalent membrane and bending coefficients of thermal expansions for symmetric laminated panel are derived and represented with lamination parameters using Classical Lamina...

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Main Authors: Peng Jin, Qihao Zheng, Wei Wei
Format: Article
Language:English
Published: Wiley 2022-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2022/5201514
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author Peng Jin
Qihao Zheng
Wei Wei
author_facet Peng Jin
Qihao Zheng
Wei Wei
author_sort Peng Jin
collection DOAJ
description This work investigates thermal aeroelastic tailoring of a laminated composite panel with a lamination parameter-based method. Equivalent membrane and bending coefficients of thermal expansions for symmetric laminated panel are derived and represented with lamination parameters using Classical Laminated Plate Theory. The relationship between thermal flutter behavior and lamination parameters is examined. The optimization process is split into two stages. In the first stage, lamination parameters and laminate thicknesses are as design variables to minimize the structure mass, subject to thermal flutter behavior and feasible region constraints of lamination parameters. In the second-stage, instead of using conventional genetic algorithm, the enhanced JAYA method is extended to search the laminate configuration to target the optimal lamination parameters. The effectiveness of the presented method is demonstrated through a thermal aeroelastic tailoring problem.
format Article
id doaj-art-c5764106c02d4248b1aa4471bb5428c6
institution Kabale University
issn 1687-5974
language English
publishDate 2022-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-c5764106c02d4248b1aa4471bb5428c62025-02-03T01:11:58ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/5201514Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA AlgorithmPeng Jin0Qihao Zheng1Wei Wei2School of Aerospace EngineeringSchool of Aerospace EngineeringSchool of Aerospace EngineeringThis work investigates thermal aeroelastic tailoring of a laminated composite panel with a lamination parameter-based method. Equivalent membrane and bending coefficients of thermal expansions for symmetric laminated panel are derived and represented with lamination parameters using Classical Laminated Plate Theory. The relationship between thermal flutter behavior and lamination parameters is examined. The optimization process is split into two stages. In the first stage, lamination parameters and laminate thicknesses are as design variables to minimize the structure mass, subject to thermal flutter behavior and feasible region constraints of lamination parameters. In the second-stage, instead of using conventional genetic algorithm, the enhanced JAYA method is extended to search the laminate configuration to target the optimal lamination parameters. The effectiveness of the presented method is demonstrated through a thermal aeroelastic tailoring problem.http://dx.doi.org/10.1155/2022/5201514
spellingShingle Peng Jin
Qihao Zheng
Wei Wei
Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
International Journal of Aerospace Engineering
title Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
title_full Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
title_fullStr Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
title_full_unstemmed Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
title_short Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
title_sort thermal aeroelastic tailoring for laminated panel with lamination parameters and jaya algorithm
url http://dx.doi.org/10.1155/2022/5201514
work_keys_str_mv AT pengjin thermalaeroelastictailoringforlaminatedpanelwithlaminationparametersandjayaalgorithm
AT qihaozheng thermalaeroelastictailoringforlaminatedpanelwithlaminationparametersandjayaalgorithm
AT weiwei thermalaeroelastictailoringforlaminatedpanelwithlaminationparametersandjayaalgorithm