Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations

Detalhes bibliográficos
Autor(a) principal: Ney Rafael Sêcco
Data de Publicação: 2014
Tipo de documento: Dissertação
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2955
Resumo: Multi-disciplinary Design Optimization highly demands computational resources, therefore it is important to develop design tools with low computational cost without compromising the fidelity of the model. The main goal of this work was to establish a methodology of training artificial neural networks for specific purposes of aircraft aerodynamic design, in order to substitute a computational fluid dynamics software in an optimization framework. This neural network would predict the lift and drag coefficients for an airliner';s wing-fuselage configuration based on its planform, airfoil, and flight condition parameters. This work also aimed to find the structure and the size of the network that best suits this problem, setting up references for future works. The aerodynamic database required for the neural network training was generated with a full-potential multiblock code. The training used the back propagation algorithm, the scaled conjugate gradient algorithm, and the Nguyen-Widrow weight initialization. Networks with different numbers of neurons were evaluated in order to minimize the regression error. The optimum networks reduced the computation time for the calculations of the aerodynamic coefficients in 4000 times when compared with the full-potential code. The average absolute errors obtained were of 0.004 and 0.0005 for lift and drag coefficients, respectively. We also propose an adapted version of the back propagation algorithm that allows the computation of gradients for optimization tasks using the artificial neural networks.
id ITA_407b5d1bee351f61a234a2fa9a828e18
oai_identifier_str oai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2955
network_acronym_str ITA
network_name_str Biblioteca Digital de Teses e Dissertações do ITA
spelling Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurationsFuselagensOtimizaçãoCoeficientes aerodinâmicosDinâmica dos fluidos computacionalEstruturas de aeronavesAerodinâmicaEngenharia aeronáuticaMulti-disciplinary Design Optimization highly demands computational resources, therefore it is important to develop design tools with low computational cost without compromising the fidelity of the model. The main goal of this work was to establish a methodology of training artificial neural networks for specific purposes of aircraft aerodynamic design, in order to substitute a computational fluid dynamics software in an optimization framework. This neural network would predict the lift and drag coefficients for an airliner';s wing-fuselage configuration based on its planform, airfoil, and flight condition parameters. This work also aimed to find the structure and the size of the network that best suits this problem, setting up references for future works. The aerodynamic database required for the neural network training was generated with a full-potential multiblock code. The training used the back propagation algorithm, the scaled conjugate gradient algorithm, and the Nguyen-Widrow weight initialization. Networks with different numbers of neurons were evaluated in order to minimize the regression error. The optimum networks reduced the computation time for the calculations of the aerodynamic coefficients in 4000 times when compared with the full-potential code. The average absolute errors obtained were of 0.004 and 0.0005 for lift and drag coefficients, respectively. We also propose an adapted version of the back propagation algorithm that allows the computation of gradients for optimization tasks using the artificial neural networks.Instituto Tecnológico de AeronáuticaBento Silva de MattosNey Rafael Sêcco2014-06-03info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2955reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:05:01Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2955http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:40:30.202Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
title Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
spellingShingle Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
Ney Rafael Sêcco
Fuselagens
Otimização
Coeficientes aerodinâmicos
Dinâmica dos fluidos computacional
Estruturas de aeronaves
Aerodinâmica
Engenharia aeronáutica
title_short Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
title_full Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
title_fullStr Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
title_full_unstemmed Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
title_sort Training artificial neural networks to predict aerodynamic coefficients of airliner wing-fuselage configurations
author Ney Rafael Sêcco
author_facet Ney Rafael Sêcco
author_role author
dc.contributor.none.fl_str_mv Bento Silva de Mattos
dc.contributor.author.fl_str_mv Ney Rafael Sêcco
dc.subject.por.fl_str_mv Fuselagens
Otimização
Coeficientes aerodinâmicos
Dinâmica dos fluidos computacional
Estruturas de aeronaves
Aerodinâmica
Engenharia aeronáutica
topic Fuselagens
Otimização
Coeficientes aerodinâmicos
Dinâmica dos fluidos computacional
Estruturas de aeronaves
Aerodinâmica
Engenharia aeronáutica
dc.description.none.fl_txt_mv Multi-disciplinary Design Optimization highly demands computational resources, therefore it is important to develop design tools with low computational cost without compromising the fidelity of the model. The main goal of this work was to establish a methodology of training artificial neural networks for specific purposes of aircraft aerodynamic design, in order to substitute a computational fluid dynamics software in an optimization framework. This neural network would predict the lift and drag coefficients for an airliner';s wing-fuselage configuration based on its planform, airfoil, and flight condition parameters. This work also aimed to find the structure and the size of the network that best suits this problem, setting up references for future works. The aerodynamic database required for the neural network training was generated with a full-potential multiblock code. The training used the back propagation algorithm, the scaled conjugate gradient algorithm, and the Nguyen-Widrow weight initialization. Networks with different numbers of neurons were evaluated in order to minimize the regression error. The optimum networks reduced the computation time for the calculations of the aerodynamic coefficients in 4000 times when compared with the full-potential code. The average absolute errors obtained were of 0.004 and 0.0005 for lift and drag coefficients, respectively. We also propose an adapted version of the back propagation algorithm that allows the computation of gradients for optimization tasks using the artificial neural networks.
description Multi-disciplinary Design Optimization highly demands computational resources, therefore it is important to develop design tools with low computational cost without compromising the fidelity of the model. The main goal of this work was to establish a methodology of training artificial neural networks for specific purposes of aircraft aerodynamic design, in order to substitute a computational fluid dynamics software in an optimization framework. This neural network would predict the lift and drag coefficients for an airliner';s wing-fuselage configuration based on its planform, airfoil, and flight condition parameters. This work also aimed to find the structure and the size of the network that best suits this problem, setting up references for future works. The aerodynamic database required for the neural network training was generated with a full-potential multiblock code. The training used the back propagation algorithm, the scaled conjugate gradient algorithm, and the Nguyen-Widrow weight initialization. Networks with different numbers of neurons were evaluated in order to minimize the regression error. The optimum networks reduced the computation time for the calculations of the aerodynamic coefficients in 4000 times when compared with the full-potential code. The average absolute errors obtained were of 0.004 and 0.0005 for lift and drag coefficients, respectively. We also propose an adapted version of the back propagation algorithm that allows the computation of gradients for optimization tasks using the artificial neural networks.
publishDate 2014
dc.date.none.fl_str_mv 2014-06-03
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/masterThesis
status_str publishedVersion
format masterThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2955
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2955
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Fuselagens
Otimização
Coeficientes aerodinâmicos
Dinâmica dos fluidos computacional
Estruturas de aeronaves
Aerodinâmica
Engenharia aeronáutica
_version_ 1706809293141966848