On the maximization of control power in low-speed flight

Detalhes bibliográficos
Autor(a) principal: Campos, L.
Data de Publicação: 2020
Outros Autores: Marques, Joaquim
Tipo de documento: Artigo de conferência
Idioma: por
Título da fonte: Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
Texto Completo: http://hdl.handle.net/10174/33705
Resumo: The present work extends existing knowledge on the subject in two directions: (i) on theoretical side by allowing for the deflections of multiple control surfaces, that gives more options to obtain the desired forces or moments with less risk of flow separation or aeroelastic effects; (ii) on the application side by considering not only minimum drag but also maximum drag (e.g. for fast descent) and maximum control moments for emergencies, such an engine-out condition. These applications are made to a FW, extending the scope of the literature that concentrates mostly on minimum drag for pitch trim in cruise. Thus the present paper is also a contribution to the expanding literature on various aspects of the BWB aircraft.
id RCAP_b43f3acc2dd31e37fdf3c3efdf6c965a
oai_identifier_str oai:dspace.uevora.pt:10174/33705
network_acronym_str RCAP
network_name_str Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
repository_id_str 7160
spelling On the maximization of control power in low-speed flightThe present work extends existing knowledge on the subject in two directions: (i) on theoretical side by allowing for the deflections of multiple control surfaces, that gives more options to obtain the desired forces or moments with less risk of flow separation or aeroelastic effects; (ii) on the application side by considering not only minimum drag but also maximum drag (e.g. for fast descent) and maximum control moments for emergencies, such an engine-out condition. These applications are made to a FW, extending the scope of the literature that concentrates mostly on minimum drag for pitch trim in cruise. Thus the present paper is also a contribution to the expanding literature on various aspects of the BWB aircraft.2023-01-30T15:50:16Z2023-01-302020-09-01T00:00:00Zinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObjecthttp://hdl.handle.net/10174/33705http://hdl.handle.net/10174/33705porShangai, ChinasimnaonaondndCampos, L.Marques, Joaquiminfo:eu-repo/semantics/openAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2024-01-03T19:35:47Zoai:dspace.uevora.pt:10174/33705Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-20T01:22:31.267751Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse
dc.title.none.fl_str_mv On the maximization of control power in low-speed flight
title On the maximization of control power in low-speed flight
spellingShingle On the maximization of control power in low-speed flight
Campos, L.
title_short On the maximization of control power in low-speed flight
title_full On the maximization of control power in low-speed flight
title_fullStr On the maximization of control power in low-speed flight
title_full_unstemmed On the maximization of control power in low-speed flight
title_sort On the maximization of control power in low-speed flight
author Campos, L.
author_facet Campos, L.
Marques, Joaquim
author_role author
author2 Marques, Joaquim
author2_role author
dc.contributor.author.fl_str_mv Campos, L.
Marques, Joaquim
description The present work extends existing knowledge on the subject in two directions: (i) on theoretical side by allowing for the deflections of multiple control surfaces, that gives more options to obtain the desired forces or moments with less risk of flow separation or aeroelastic effects; (ii) on the application side by considering not only minimum drag but also maximum drag (e.g. for fast descent) and maximum control moments for emergencies, such an engine-out condition. These applications are made to a FW, extending the scope of the literature that concentrates mostly on minimum drag for pitch trim in cruise. Thus the present paper is also a contribution to the expanding literature on various aspects of the BWB aircraft.
publishDate 2020
dc.date.none.fl_str_mv 2020-09-01T00:00:00Z
2023-01-30T15:50:16Z
2023-01-30
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/conferenceObject
format conferenceObject
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://hdl.handle.net/10174/33705
http://hdl.handle.net/10174/33705
url http://hdl.handle.net/10174/33705
dc.language.iso.fl_str_mv por
language por
dc.relation.none.fl_str_mv Shangai, China
sim
nao
nao
nd
nd
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.source.none.fl_str_mv reponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação
instacron:RCAAP
instname_str Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação
instacron_str RCAAP
institution RCAAP
reponame_str Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
collection Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
repository.name.fl_str_mv Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação
repository.mail.fl_str_mv
_version_ 1817553436483256320

Registros relacionados