Zitierlink: https://doi.org/10.48441/4427.2474
Volltextdatei(en) in REPOSIT vorhanden Open Access https://creativecommons.org/licenses/by-nc-sa/4.0/
DC ElementWertSprache
dc.contributor.authorCaja Calleja, Ricardo-
dc.contributor.authorSchiktanz, Daniel-
dc.contributor.authorScholz, Dieter-
dc.date.accessioned2025-05-16T10:12:54Z-
dc.date.available2025-05-16T10:12:54Z-
dc.date.issued2011-11-24-
dc.identifier.urihttps://hdl.handle.net/20.500.12738/17590-
dc.description.abstractThis presentation shows a flight dynamics analysis of the Box Wing Aircraft (BWA) configuration. Aim of the BWA is a reduction of induced drag. The flight dynamics analysis of an aircraft within the conceptual design stage is necessary to decide as soon as possible whether its design is feasible (the aircraft will behave properly). An automatic workflow for analysing aircraft with multiple wings is not possible within CEASIOM. Hence the aerodynamic modules are used as standalone applications (Digital Datcom, Tornado…). Once the derivatives were known the flying and handling qualities of the aircraft could be examined, and a decision about the validity of the design could be made.en
dc.description.sponsorshipBundesministerium für Forschung, Technologie und Raumfahrten_US
dc.language.isoenen_US
dc.subjectaviationen_US
dc.subjectaircraften_US
dc.subjectpassengeren_US
dc.subjectairporten_US
dc.subject2030en_US
dc.subjectBox Wing Aircraften_US
dc.subjectBWAen_US
dc.subjectpreliminaryen_US
dc.subjectconceptualen_US
dc.subjectdesignen_US
dc.subjectconfigurationen_US
dc.subjectdragen_US
dc.subjectflighten_US
dc.subjectdynamicsen_US
dc.subjectwingen_US
dc.subjectCEASIOMen_US
dc.subjectaerodynamicsen_US
dc.subjectdigitalen_US
dc.subjectDatcomen_US
dc.subjectTornadoen_US
dc.subjectJSBSimen_US
dc.subjectFlight Gearen_US
dc.subjectstabilityen_US
dc.subjectcontrolen_US
dc.subjectderivativeen_US
dc.subjecteigenmodeen_US
dc.subjectphugoiden_US
dc.subjectshort perioden_US
dc.subjectoscillationen_US
dc.subjectflyingen_US
dc.subjecthandlingen_US
dc.subjectqualitiesen_US
dc.subjectCooperen_US
dc.subjectHarperen_US
dc.subjectrating scaleen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleFlight dynamics analysis of a medium range box wing aircraften
dc.typePresentationen_US
dc.relation.conferenceSpanish Space Students Congress 2011en_US
dc.identifier.doi10.48441/4427.2474-
dc.description.versionNonPeerRevieweden_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-212101-
tuhh.oai.showtrueen_US
tuhh.publication.instituteForschungsgruppe Flugzeugentwurf und -systeme (AERO)en_US
tuhh.publication.instituteDepartment Fahrzeugtechnik und Flugzeugbauen_US
tuhh.publication.instituteFakultät Technik und Informatiken_US
tuhh.publisher.urlhttps://www.fzt.haw-hamburg.de/pers/Scholz/Airport2030/Airport2030_PRE_6thS3_11-11-24.pdf-
tuhh.type.opusPräsentation-
tuhh.type.rdmtrue-
dc.relation.projectSpitzencluster Luftfahrt - Metropolregion Hamburg; Teilprojekt 3: Effizienter Flughafen 2030en_US
dc.rights.cchttps://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.type.casraiOther-
dc.type.diniOther-
dc.type.driverother-
dc.type.statusinfo:eu-repo/semantics/publishedVersionen_US
dcterms.DCMITypeInteractiveResource-
local.comment.externalCAJA CALLEJA, Ricardo, SCHIKTANZ, Daniel, SCHOLZ, Dieter, 2011. Flight Dynamics Analysis of a Medium Range Box Wing Aircraft. In: VI Spanish Space Students Congress (Las Palmas, Spain, 24-25 November 2011). Available from: https://doi.org/10.48441/4427.2474en_US
tuhh.apc.statusfalseen_US
item.fulltextWith Fulltext-
item.openairetypePresentation-
item.creatorOrcidCaja Calleja, Ricardo-
item.creatorOrcidSchiktanz, Daniel-
item.creatorOrcidScholz, Dieter-
item.grantfulltextopen-
item.openairecristypehttp://purl.org/coar/resource_type/c_c94f-
item.languageiso639-1en-
item.creatorGNDCaja Calleja, Ricardo-
item.creatorGNDSchiktanz, Daniel-
item.creatorGNDScholz, Dieter-
item.cerifentitytypePublications-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.orcid0000-0002-8188-7269-
crisitem.author.parentorgFakultät Technik und Informatik-
crisitem.project.funderBundesministerium für Forschung, Technologie und Raumfahrt-
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