Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.2134
Fulltext available Open Access https://creativecommons.org/licenses/by-nc-sa/4.0/
DC FieldValueLanguage
dc.contributor.authorKrull, Marlis-
dc.contributor.authorScholz, Dieter-
dc.date.accessioned2024-12-10T09:28:18Z-
dc.date.available2024-12-10T09:28:18Z-
dc.date.issued2024-09-30-
dc.identifier.urihttps://hdl.handle.net/20.500.12738/16687-
dc.description.abstractPropeller driven aircraft have a higher propulsive efficiency, less drag, less Direct Operating Costs (DOC), and much less equivalent CO2 due to contrail avoidance at lower cruise altitude compared to traditional passenger jet aircraft. Accordingly, large propeller aircraft should be the choice for the next generation of aircraft to replace current passenger jets. For this reason, we teach such designs at HAW Hamburg based on our PhD-level research.en
dc.language.isoenen_US
dc.subjectLuftfahrten_US
dc.subjectLuftfahrzeugen_US
dc.subjectTriebwerken_US
dc.subjectPropelleren_US
dc.subjectFlugzeugen_US
dc.subjectFlugtriebwerken_US
dc.subjectTurboluftstrahltriebwerken_US
dc.subjectEntwurfen_US
dc.subjectTabellenkalkulationen_US
dc.subjectOptimierungen_US
dc.subjectAeronauticsen_US
dc.subjectAirplanesen_US
dc.subjectMotorsen_US
dc.subjectPropellersen_US
dc.subjectSpreadsheetsen_US
dc.subjectDesignen_US
dc.subjectConstructionen_US
dc.subjectTurbinesen_US
dc.subjectMathematical optimizationen_US
dc.subjectMach numberen_US
dc.subjectEngineen_US
dc.subjectAircraften_US
dc.subjectSizingen_US
dc.subjectEfficiencyen_US
dc.subjectATRen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titlePreliminary sizing and optimization of propeller aircraft (Part 25)en
dc.typePosteren_US
dc.relation.conferenceDeutscher Luft- und Raumfahrtkongress 2024en_US
dc.identifier.doi10.48441/4427.2134-
dc.description.versionNonPeerRevieweden_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-199987-
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://purl.org/aero/POS2024-09-30j-
tuhh.publisher.urlhttps://publikationen.dglr.de/?tx_dglrpublications_pi1[document_id]=630513-
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.IsSupplementedByurn:urn:nbn:de:gbv:18302-aero2022-04-29.012en_US
datacite.relation.IsSupplementedBydoi:10.7910/DVN/ET4ZKVen_US
local.comment.externalKRULL, Marlis, SCHOLZ, Dieter, 2024. Preliminary Sizing and Optimization of Propeller Aircraft (Part 25). Poster. German Aerospace Congress (Hamburg, 30.09. - 02.10.2024). Available from: https://doi.org/10.48441/4427.2134en_US
tuhh.apc.statusfalseen_US
item.creatorGNDKrull, Marlis-
item.creatorGNDScholz, Dieter-
item.fulltextWith Fulltext-
item.creatorOrcidKrull, Marlis-
item.creatorOrcidScholz, Dieter-
item.grantfulltextopen-
item.cerifentitytypePublications-
item.languageiso639-1en-
item.openairecristypehttp://purl.org/coar/resource_type/c_6670-
item.openairetypePoster-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.orcid0000-0002-8188-7269-
crisitem.author.parentorgFakultät Technik und Informatik-
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