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An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique

Bibliographic Details
Main Author: Jung,SungKi
Publication Date: 2016
Other Authors: Choi,Won, Martins-Filho,Luiz S., Madeira,Fernando
Format: Article
Language: eng
Source: Journal of Aerospace Technology and Management (Online)
Download full: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000200193
Summary: ABSTRACT Design candidates obtained from optimization techniques may have meaningful information, which provides not only the best solution, but also a relationship between object functions and design variables. In particular, trade-off studies for optimum airfoil shape design involving various objectives and design variables require the effective analysis tool to take into account a complexity between objectives and design variables. In this study, for the multiple-conflicting objectives that need to be simultaneously fulfilled, the real-coded Adaptive Range Multi-Objective Genetic Algorithm code, which represents the global and stochastic multi-objective evolutionary algorithm, was developed for an airfoil shape design. Furthermore, the PARSEC method reflecting geometrical properties of airfoil is adopted to generate airfoil shapes. In addition, the Self-Organizing Maps, based on the neural network, are used to visualize trade-offs of a relationship between the objective function space and the design variable space obtained by evolutionary computation. The Self-Organizing Maps that can be considered as data mining of the engineering design generate clusters of object functions and design variables as an essential role of trade-off studies. The aerodynamic data for all candidate airfoils is obtained through Computational Fluid Dynamics. Lastly, the relationship between the maximum lift coefficient and maximum lift-to-drag ratio as object functions and 12 airfoil design parameters based on the PARSEC method is investigated using the Self-Organizing Maps method.
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spelling An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization TechniqueAerodynamicsAdaptive Range Multi-Object Genetic AlgorithmPARSECSelf-Organizing MapComputational Fluid DynamicsABSTRACT Design candidates obtained from optimization techniques may have meaningful information, which provides not only the best solution, but also a relationship between object functions and design variables. In particular, trade-off studies for optimum airfoil shape design involving various objectives and design variables require the effective analysis tool to take into account a complexity between objectives and design variables. In this study, for the multiple-conflicting objectives that need to be simultaneously fulfilled, the real-coded Adaptive Range Multi-Objective Genetic Algorithm code, which represents the global and stochastic multi-objective evolutionary algorithm, was developed for an airfoil shape design. Furthermore, the PARSEC method reflecting geometrical properties of airfoil is adopted to generate airfoil shapes. In addition, the Self-Organizing Maps, based on the neural network, are used to visualize trade-offs of a relationship between the objective function space and the design variable space obtained by evolutionary computation. The Self-Organizing Maps that can be considered as data mining of the engineering design generate clusters of object functions and design variables as an essential role of trade-off studies. The aerodynamic data for all candidate airfoils is obtained through Computational Fluid Dynamics. Lastly, the relationship between the maximum lift coefficient and maximum lift-to-drag ratio as object functions and 12 airfoil design parameters based on the PARSEC method is investigated using the Self-Organizing Maps method.Departamento de Ciência e Tecnologia Aeroespacial2016-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000200193Journal of Aerospace Technology and Management v.8 n.2 2016reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v8i2.585info:eu-repo/semantics/openAccessJung,SungKiChoi,WonMartins-Filho,Luiz S.Madeira,Fernandoeng2016-08-02T00:00:00Zoai:scielo:S2175-91462016000200193Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2016-08-02T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
title An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
spellingShingle An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
Jung,SungKi
Aerodynamics
Adaptive Range Multi-Object Genetic Algorithm
PARSEC
Self-Organizing Map
Computational Fluid Dynamics
title_short An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
title_full An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
title_fullStr An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
title_full_unstemmed An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
title_sort An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique
author Jung,SungKi
author_facet Jung,SungKi
Choi,Won
Martins-Filho,Luiz S.
Madeira,Fernando
author_role author
author2 Choi,Won
Martins-Filho,Luiz S.
Madeira,Fernando
author2_role author
author
author
dc.contributor.author.fl_str_mv Jung,SungKi
Choi,Won
Martins-Filho,Luiz S.
Madeira,Fernando
dc.subject.por.fl_str_mv Aerodynamics
Adaptive Range Multi-Object Genetic Algorithm
PARSEC
Self-Organizing Map
Computational Fluid Dynamics
topic Aerodynamics
Adaptive Range Multi-Object Genetic Algorithm
PARSEC
Self-Organizing Map
Computational Fluid Dynamics
description ABSTRACT Design candidates obtained from optimization techniques may have meaningful information, which provides not only the best solution, but also a relationship between object functions and design variables. In particular, trade-off studies for optimum airfoil shape design involving various objectives and design variables require the effective analysis tool to take into account a complexity between objectives and design variables. In this study, for the multiple-conflicting objectives that need to be simultaneously fulfilled, the real-coded Adaptive Range Multi-Objective Genetic Algorithm code, which represents the global and stochastic multi-objective evolutionary algorithm, was developed for an airfoil shape design. Furthermore, the PARSEC method reflecting geometrical properties of airfoil is adopted to generate airfoil shapes. In addition, the Self-Organizing Maps, based on the neural network, are used to visualize trade-offs of a relationship between the objective function space and the design variable space obtained by evolutionary computation. The Self-Organizing Maps that can be considered as data mining of the engineering design generate clusters of object functions and design variables as an essential role of trade-off studies. The aerodynamic data for all candidate airfoils is obtained through Computational Fluid Dynamics. Lastly, the relationship between the maximum lift coefficient and maximum lift-to-drag ratio as object functions and 12 airfoil design parameters based on the PARSEC method is investigated using the Self-Organizing Maps method.
publishDate 2016
dc.date.none.fl_str_mv 2016-06-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000200193
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000200193
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v8i2.585
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.8 n.2 2016
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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