Close

1. Identity statement
Reference TypeJournal Article
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/36HKRTH
Repositorysid.inpe.br/mtc-m19@80/2009/12.09.16.10   (restricted access)
Last Update2009:12.09.16.10.16 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19@80/2009/12.09.16.10.17
Metadata Last Update2018:06.05.04.35.59 (UTC) administrator
Secondary KeyINPE--PRE/
DOI10.1007/s00158-009-0429-6
ISSN1615-147X
1615-1488
Citation KeyGasbarriChiwCamp:2009:HyMuAp
TitleA hybrid multilevel approach for aeroelastic optimization of composite wing-box
Year2009
MonthAug.
Access Date2024, Apr. 28
Secondary TypePRE PI
Number of Files1
Size826 KiB
2. Context
Author1 Gasbarri, Paolo
2 Chiwiacosky, Leonardo D.
3 Campos Velho, Haroldo Fraga de
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JHC3
Group1
2
3 LAC-CTE-INPE-MCT-BR
Affiliation1 Università degli Studi di Roma
2 Universidade do Vale do Rio dos Sinos (UNISINOS)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
JournalStructural and Multidisciplinary Optimization
Volume39
Number6
Pages607-624
Secondary MarkA1_ENGENHARIAS_I B1_ENGENHARIAS_III
History (UTC)2009-12-09 16:33:56 :: simone -> administrator ::
2018-06-05 04:35:59 :: administrator -> marciana :: 2009
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsStructural optimization - Multilevel optimization - Composite structures - Genetic algorithm
AbstractThe quest for finding optimum solutions to engineering problems has been existing for a long time. In the last decade several optimization techniques have been applied to the structural design of composite wing structures. Generally many of these proposed procedures have dealt with different disciplines such as aerodynamics, structures, or dynamics separately. However an aeronautical design process is multidisciplinary since it involves strong couplings and interactions among, for instance, aerodynamics, dynamics, flight mechanics and structures. The main problem in a multidisciplinary aircraft design is usually the development of an efficient method to integrate structures or structural properties, which can be considered both as global and local design variables. This paper describes an integrated aerodynamic / dynamic / structural optimization procedure for a composite wing-box design. The procedure combines an aeroelastic optimization of a composite wing based on a general purpose optimizer such as the Sequential Quadratic Programming (SQP) and a composite optimization using Genetic Algorithm (GA). Both the optimizations are implemented through a hybrid multilevel decomposition technique.
AreaCOMP
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > A hybrid multilevel...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filehybrid.pdf
User Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
Next Higher Units8JMKD3MGPCW/3ESGTTP
DisseminationWEBSCI
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel documentstage e-mailaddress electronicmailaddress format isbn label lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype
7. Description control
e-Mail (login)marciana
update 


Close