VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS

Detalhes bibliográficos
Autor(a) principal: ANGELO ANTONIO VERRI
Data de Publicação: 2020
Tipo de documento: Tese
Título da fonte: Portal de Dados Abertos da CAPES
Texto Completo: https://sucupira.capes.gov.br/sucupira/public/consultas/coleta/trabalhoConclusao/viewTrabalhoConclusao.jsf?popup=true&id_trabalho=9536043
id BRCRIS_dc259a12888480a35b5e79d1dc61fb6b
network_acronym_str CAPES
network_name_str Portal de Dados Abertos da CAPES
dc.title.pt-BR.fl_str_mv VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
title VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
spellingShingle VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
ENGENHARIA ESTRUTURAL
STATIC AEROELASTICITY
ANGELO ANTONIO VERRI
title_short VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
title_full VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
title_fullStr VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
title_full_unstemmed VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
title_sort VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS
topic ENGENHARIA ESTRUTURAL
STATIC AEROELASTICITY
publishDate 2020
format doctoralThesis
url https://sucupira.capes.gov.br/sucupira/public/consultas/coleta/trabalhoConclusao/viewTrabalhoConclusao.jsf?popup=true&id_trabalho=9536043
author_role author
author ANGELO ANTONIO VERRI
author_facet ANGELO ANTONIO VERRI
dc.contributor.authorLattes.fl_str_mv http://lattes.cnpq.br/9122058134476998
dc.identifier.orcid.none.fl_str_mv https://orcid.org/0000-0001-9004-2164
dc.contributor.advisor1.fl_str_mv FLAVIO LUIZ DE SILVA BUSSAMRA
dc.contributor.advisor1Lattes.fl_str_mv http://lattes.cnpq.br/0616738413255391
dc.publisher.none.fl_str_mv INSTITUTO TECNOLÓGICO DE AERONÁUTICA
publisher.none.fl_str_mv INSTITUTO TECNOLÓGICO DE AERONÁUTICA
instname_str INSTITUTO TECNOLÓGICO DE AERONÁUTICA
dc.publisher.program.fl_str_mv ENGENHARIA AERONÂUTICA E MECÂNICA
dc.description.course.none.fl_txt_mv ENGENHARIA AERONÂUTICA E MECÂNICA
reponame_str Portal de Dados Abertos da CAPES
collection Portal de Dados Abertos da CAPES
spelling CAPESPortal de Dados Abertos da CAPESVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSVERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTSENGENHARIA ESTRUTURAL2020doctoralThesishttps://sucupira.capes.gov.br/sucupira/public/consultas/coleta/trabalhoConclusao/viewTrabalhoConclusao.jsf?popup=true&id_trabalho=9536043authorANGELO ANTONIO VERRIhttp://lattes.cnpq.br/9122058134476998https://orcid.org/0000-0001-9004-2164FLAVIO LUIZ DE SILVA BUSSAMRAhttp://lattes.cnpq.br/0616738413255391INSTITUTO TECNOLÓGICO DE AERONÁUTICAINSTITUTO TECNOLÓGICO DE AERONÁUTICAINSTITUTO TECNOLÓGICO DE AERONÁUTICAENGENHARIA AERONÂUTICA E MECÂNICAENGENHARIA AERONÂUTICA E MECÂNICAPortal de Dados Abertos da CAPESPortal de Dados Abertos da CAPES
identifier_str_mv VERRI, ANGELO ANTONIO. VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS. 2020. Tese.
dc.identifier.citation.fl_str_mv VERRI, ANGELO ANTONIO. VERY FLEXIBLE WING STRUCTURAL ANALYSIS CONSIDERING NONLINEAR STATIC AEROELASTIC EFFECTS. 2020. Tese.
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