A new sonic box formulation for oscillating swept thick wings in transonic flow.
| Autor(a) principal: | |
|---|---|
| Data de Publicação: | 2004 |
| 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=86 |
Resumo: | The present work shows a mathematical model for unsteady linearized potential flow around thin wings having swept leading and trailing edges and over thick wings with swept and unswept leading edges. Doublet integrals are obtained for the three dimensional case. The wings are supposed to be describing small amplitude harmonic motions of pitch and plunge. Exact solutions for thin and thick wings oscillating on an unsteady potential sonic flow are presented and are compared with other works. |
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Biblioteca Digital de Teses e Dissertações do ITA |
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A new sonic box formulation for oscillating swept thick wings in transonic flow.Aerodinâmica não-estacionáriaMétodo dos painéis (dinâmica dos fluídos)Escoamento transônicoAsasPlacas espessasModelos matemáticosFísicaEngenharia aeronáuticaThe present work shows a mathematical model for unsteady linearized potential flow around thin wings having swept leading and trailing edges and over thick wings with swept and unswept leading edges. Doublet integrals are obtained for the three dimensional case. The wings are supposed to be describing small amplitude harmonic motions of pitch and plunge. Exact solutions for thin and thick wings oscillating on an unsteady potential sonic flow are presented and are compared with other works. Instituto Tecnológico de AeronáuticaPaulo Afonso de Oliveira SovieroGuilherme Augusto Vargas Cesar2004-00-00info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=86reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:01:38Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:86http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:32:11.305Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
| dc.title.none.fl_str_mv |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| title |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| spellingShingle |
A new sonic box formulation for oscillating swept thick wings in transonic flow. Guilherme Augusto Vargas Cesar Aerodinâmica não-estacionária Método dos painéis (dinâmica dos fluídos) Escoamento transônico Asas Placas espessas Modelos matemáticos Física Engenharia aeronáutica |
| title_short |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| title_full |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| title_fullStr |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| title_full_unstemmed |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| title_sort |
A new sonic box formulation for oscillating swept thick wings in transonic flow. |
| author |
Guilherme Augusto Vargas Cesar |
| author_facet |
Guilherme Augusto Vargas Cesar |
| author_role |
author |
| dc.contributor.none.fl_str_mv |
Paulo Afonso de Oliveira Soviero |
| dc.contributor.author.fl_str_mv |
Guilherme Augusto Vargas Cesar |
| dc.subject.por.fl_str_mv |
Aerodinâmica não-estacionária Método dos painéis (dinâmica dos fluídos) Escoamento transônico Asas Placas espessas Modelos matemáticos Física Engenharia aeronáutica |
| topic |
Aerodinâmica não-estacionária Método dos painéis (dinâmica dos fluídos) Escoamento transônico Asas Placas espessas Modelos matemáticos Física Engenharia aeronáutica |
| dc.description.none.fl_txt_mv |
The present work shows a mathematical model for unsteady linearized potential flow around thin wings having swept leading and trailing edges and over thick wings with swept and unswept leading edges. Doublet integrals are obtained for the three dimensional case. The wings are supposed to be describing small amplitude harmonic motions of pitch and plunge. Exact solutions for thin and thick wings oscillating on an unsteady potential sonic flow are presented and are compared with other works. |
| description |
The present work shows a mathematical model for unsteady linearized potential flow around thin wings having swept leading and trailing edges and over thick wings with swept and unswept leading edges. Doublet integrals are obtained for the three dimensional case. The wings are supposed to be describing small amplitude harmonic motions of pitch and plunge. Exact solutions for thin and thick wings oscillating on an unsteady potential sonic flow are presented and are compared with other works. |
| publishDate |
2004 |
| dc.date.none.fl_str_mv |
2004-00-00 |
| 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=86 |
| url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=86 |
| 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 |
Aerodinâmica não-estacionária Método dos painéis (dinâmica dos fluídos) Escoamento transônico Asas Placas espessas Modelos matemáticos Física Engenharia aeronáutica |
| _version_ |
1706809252697341952 |