Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.558
Fulltext available Open Access https://creativecommons.org/licenses/by-nc-sa/4.0/
DC FieldValueLanguage
dc.contributor.authorCamilo, Denis-
dc.contributor.authorGaihre, Pankaj-
dc.contributor.authorScholz, Dieter-
dc.date.accessioned2022-09-26T12:03:43Z-
dc.date.available2022-09-26T12:03:43Z-
dc.date.issued2022-09-26-
dc.identifier.urihttp://hdl.handle.net/20.500.12738/13322-
dc.description.abstractEvery aircraft produces wake turbulence during flight. The strength of wake turbulence depends on various factors, for example aircraft mass, wingspan, speed or wing geometry. However, FAA, EUROCONTROL and ICAO consider only aircraft mass and wingspan for categorization of aircraft wake turbulence. In this approach, other variables related to flight mechanics and aircraft design are used to calculate induced power. Based on these calculations, new aircraft wake turbulence categories are presented and compared to FAA, EUROCONTROL and ICAO categories.en
dc.language.isoenen_US
dc.subjectwakeen_US
dc.subjectturbulenceen_US
dc.subjectflight mechanicsen_US
dc.subjectvortexen_US
dc.subjectliften_US
dc.subjectOswald factoren_US
dc.subjectwingspanen_US
dc.subjectapproach speeden_US
dc.subjectEUROCONTROLen_US
dc.subjectICAOen_US
dc.subjectFAAen_US
dc.subjectinduced poweren_US
dc.subjectwake turbulence catagoriesen_US
dc.subjectWTCen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleComparing aircraft wake turbulence with induced power calculationsen
dc.typePosteren_US
dc.relation.conferenceDeutscher Luft- und Raumfahrtkongress 2022en_US
dc.identifier.doi10.48441/4427.558-
dc.description.versionNonPeerRevieweden_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-150662-
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://publikationen.dglr.de/?tx_dglrpublications_pi1[document_id]=570488-
tuhh.type.opusPoster-
tuhh.type.rdmtrue-
dc.rights.cchttps://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.type.casraiConference Poster-
dc.type.diniOther-
dc.type.driverother-
dc.type.statusinfo:eu-repo/semantics/publishedVersionen_US
dcterms.DCMITypeImage-
datacite.relation.IsSupplementedBydoi:10.48441/4427.402en_US
tuhh.apc.statusfalseen_US
item.creatorGNDCamilo, Denis-
item.creatorGNDGaihre, Pankaj-
item.creatorGNDScholz, Dieter-
item.languageiso639-1en-
item.cerifentitytypePublications-
item.openairecristypehttp://purl.org/coar/resource_type/c_6670-
item.creatorOrcidCamilo, Denis-
item.creatorOrcidGaihre, Pankaj-
item.creatorOrcidScholz, Dieter-
item.fulltextWith Fulltext-
item.grantfulltextopen-
item.openairetypePoster-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.orcid0000-0002-8188-7269-
crisitem.author.parentorgFakultät Technik und Informatik-
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