DC ElementWertSprache
dc.contributor.authorNiţă, Mihaela-
dc.contributor.authorScholz, Dieter-
dc.date.accessioned2020-08-26T09:16:39Z-
dc.date.available2020-08-26T09:16:39Z-
dc.date.issued2013-
dc.identifier.issn1454-2358en_US
dc.identifier.urihttp://hdl.handle.net/20.500.12738/1222-
dc.description.abstractThis paper conducts an investigation towards main aircraft cabin parameters. The aim is two-fold: First, a handbook method is used to preliminarily design the aircraft cabin. Second, an objective function representing the "drag in the responsibility of the cabin" is created and optimized using both an analytical approach and a stochastic approach. Several methods for estimating wetted area and mass are investigated. The results provide optimum values for the fuselage slenderness parameter (fuselage length divided by fuselage diameter) for civil transport aircraft. For passenger aircraft, cabin surface area is of importance. The related optimum slenderness parameter should be about 10. Optimum slenderness parameters for freighters are lower: about 8 if transport volume is of importance and about 4 if frontal area for large items to be carried is of importance. These results are published in two parts. Part I includes the handbook method for preliminarily designing the aircraft cabin. Part II includes the results of the optimization and the investigations of the wetted areas, masses and "drag in the responsibility of the cabin".en
dc.language.isoenen_US
dc.publisherUniversitatea Politehnica din Bucureştien_US
dc.relation.ispartofScientific bulletin / University Politehnica of Bucharest = Buletin ştiinţific / Universitatea Politehnica din Bucureşti. Series D, Mechanical engineeringen_US
dc.subjectevolutionary algorithmsen_US
dc.subjectoptimizationen_US
dc.subjectpreliminary cabin designen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleFrom preliminary aircraft cabin design to cabin optimization - part 2en
dc.typeArticleen_US
dc.identifier.doi10.48441/4427.2596-
dc.description.versionPeerRevieweden_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.container.endpage46en_US
tuhh.container.issue4en_US
tuhh.container.startpage27en_US
tuhh.container.volume75en_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-12169-
tuhh.oai.showtrueen_US
tuhh.publication.instituteDepartment Fahrzeugtechnik und Flugzeugbauen_US
tuhh.publication.instituteFakultät Technik und Informatiken_US
tuhh.publication.instituteForschungsgruppe Flugzeugentwurf und -systeme (AERO)en_US
tuhh.publisher.urlhttp://www.fzt.haw-hamburg.de/pers/Scholz/CARISMA/CARISMA_PUB_UPB-Sci-Bull-D-75-4_13-10-01.pdf-
tuhh.publisher.urlhttp://www.scientificbulletin.upb.ro/rev_docs_arhiva/rez074_347413.pdf-
tuhh.type.opus(wissenschaftlicher) Artikel-
dc.relation.projectCARISMA - Aircraft Cabin and Cabin System Refurbishing, Optimization of Technical Processesen_US
dc.type.casraiJournal Article-
dc.type.diniarticle-
dc.type.driverarticle-
dc.type.statusinfo:eu-repo/semantics/publishedVersionen_US
dcterms.DCMITypeText-
local.comment.externalNIŢĂ, Mihaela, SCHOLZ, Dieter, 2013. From Preliminary Aircraft Cabin Design to Cabin Optimization - Part 2. In: University Politehnica of Bucharest, Scientific Bulletin. Series D, vol. 75, no. 4, pp. 27-46. Available from: https://www.scientificbulletin.upb.ro/rev_docs_arhiva/rez074_347413.pdf, http://hdl.handle.net/20.500.12738/1222en_US
tuhh.apc.statusfalseen_US
item.creatorGNDNiţă, Mihaela-
item.creatorGNDScholz, Dieter-
item.grantfulltextopen-
item.openairetypeArticle-
item.fulltextWith Fulltext-
item.languageiso639-1en-
item.cerifentitytypePublications-
item.creatorOrcidNiţă, Mihaela-
item.creatorOrcidScholz, Dieter-
item.openairecristypehttp://purl.org/coar/resource_type/c_6501-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.orcid0000-0002-8188-7269-
crisitem.author.parentorgFakultät Technik und Informatik-
Enthalten in den Sammlungen:Publications with full text
Dateien zu dieser Ressource:
Datei Beschreibung GrößeFormat
CARISMA_PUB_UPB-Sci-Bull-D-75-4_13-10-01.pdf812.64 kBAdobe PDFÖffnen/Anzeigen
Zur Kurzanzeige

Seitenansichten

113
checked on 22.06.2025

Google ScholarTM

Prüfe

HAW Katalog

Prüfe

Feedback zu diesem Datensatz


Alle Ressourcen in diesem Repository sind urheberrechtlich geschützt.