Please use this identifier to cite or link to this item:
https://doi.org/10.48441/4427.2475
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Johanning, Andreas | - |
dc.contributor.author | Scholz, Dieter | - |
dc.date.accessioned | 2025-05-16T12:06:35Z | - |
dc.date.available | 2025-05-16T12:06:35Z | - |
dc.date.issued | 2014-06-06 | - |
dc.identifier.uri | https://hdl.handle.net/20.500.12738/17591 | - |
dc.description.abstract | The project showed the importance for gound handling to be robust. Gound handling is not the financial game changer in aircraft design. Span limitations for short-medium range aircraft of 36 m at airports drives the design (ICAO). The standard jet configuration can be optimized, if is Top Level Aircraft Requirements (TLAR) are challenged. Examples are take-off distance (longer) and cruise Mach number (slower). The best Box Wing Aircraft (BWA) configuration may be a rather conventional one with tail aft and a wing configuration similar to a biplane but with wing sweep as required for cruise Mach number. The proposed configuration is the "Smart Turboprop" especially combined with a braced wing and partial natural laminar flow on the wing. This aircraft configuration offers substantial fuel savings and DOC improvements. | en |
dc.description.sponsorship | Bundesministerium für Forschung, Technologie und Raumfahrt | en_US |
dc.language.iso | en | en_US |
dc.subject | aviation | en_US |
dc.subject | jet | en_US |
dc.subject | propeller | en_US |
dc.subject | aircraft | en_US |
dc.subject | passenger | en_US |
dc.subject | short-medium | en_US |
dc.subject | range | en_US |
dc.subject | ground | en_US |
dc.subject | handling | en_US |
dc.subject | ground handling | en_US |
dc.subject | conceptual | en_US |
dc.subject | design | en_US |
dc.subject | configuration | en_US |
dc.subject | wing | en_US |
dc.subject | braced | en_US |
dc.subject | sweep | en_US |
dc.subject | span | en_US |
dc.subject | limitation | en_US |
dc.subject | ICAO | en_US |
dc.subject | TLAR | en_US |
dc.subject | optimization | en_US |
dc.subject | Box Wing Aircraft | en_US |
dc.subject | BWA | en_US |
dc.subject | Smart Turboprop | en_US |
dc.subject | cruise | en_US |
dc.subject | Mach number | en_US |
dc.subject | natural laminar flow | en_US |
dc.subject | fuel | en_US |
dc.subject | Direct Operating Costs | en_US |
dc.subject | DOC | en_US |
dc.subject | Airbus | en_US |
dc.subject | A320 | en_US |
dc.subject | optimization | en_US |
dc.subject | box wing | en_US |
dc.subject | diamond | en_US |
dc.subject | biplane | en_US |
dc.subject | aerodynamics | en_US |
dc.subject | cabin | en_US |
dc.subject | fuselage | en_US |
dc.subject | drag | en_US |
dc.subject | family | en_US |
dc.subject | turboprop | en_US |
dc.subject | winglet | en_US |
dc.subject | airport | en_US |
dc.subject.ddc | 620: Ingenieurwissenschaften | en_US |
dc.title | Airport2030 – AP4.1 : configuration for scenario 2015 (possible A320 successor) | en |
dc.type | Presentation | en_US |
dc.relation.conference | Flugzeugkonfigurationen für effiziente Bodenoperationen 2014 | en_US |
dc.identifier.doi | 10.48441/4427.2475 | - |
dc.description.version | NonPeerReviewed | en_US |
openaire.rights | info:eu-repo/semantics/openAccess | en_US |
tuhh.identifier.urn | urn:nbn:de:gbv:18302-reposit-212129 | - |
tuhh.oai.show | true | en_US |
tuhh.publication.institute | Forschungsgruppe Flugzeugentwurf und -systeme (AERO) | en_US |
tuhh.publication.institute | Department Fahrzeugtechnik und Flugzeugbau | en_US |
tuhh.publication.institute | Fakultät Technik und Informatik | en_US |
tuhh.publisher.url | https://www.fzt.haw-hamburg.de/pers/Scholz/Airport2030/Airport2030_PRE_FinalPresentation_Airbus_2014-06-05.pdf | - |
tuhh.type.opus | Präsentation | - |
tuhh.type.rdm | true | - |
dc.relation.project | Spitzencluster Luftfahrt - Metropolregion Hamburg; Teilprojekt 3: Effizienter Flughafen 2030 | en_US |
dc.rights.cc | https://creativecommons.org/licenses/by-nc-sa/4.0/ | en_US |
dc.type.casrai | Other | - |
dc.type.dini | Other | - |
dc.type.driver | other | - |
dc.type.status | info:eu-repo/semantics/publishedVersion | en_US |
dcterms.DCMIType | InteractiveResource | - |
local.comment.external | JOHANNING, Andreas, SCHOLZ, Dieter, 2014. Airport2030 – AP4.1: Configuration for Scenario 2015 (Possible A320 Successor). In: Flugzeugkonfigurationen für effiziente Bodenoperationen (Airbus, Hamburg-Finkenwerder, 05.06.2014). Available from: https://doi.org/10.48441/4427.2475 | en_US |
tuhh.apc.status | false | en_US |
item.creatorGND | Johanning, Andreas | - |
item.creatorGND | Scholz, Dieter | - |
item.grantfulltext | open | - |
item.openairetype | Presentation | - |
item.fulltext | With Fulltext | - |
item.languageiso639-1 | en | - |
item.cerifentitytype | Publications | - |
item.creatorOrcid | Johanning, Andreas | - |
item.creatorOrcid | Scholz, Dieter | - |
item.openairecristype | http://purl.org/coar/resource_type/c_c94f | - |
crisitem.author.dept | Department Fahrzeugtechnik und Flugzeugbau | - |
crisitem.author.orcid | 0000-0002-8188-7269 | - |
crisitem.author.parentorg | Fakultät Technik und Informatik | - |
crisitem.project.funder | Bundesministerium für Forschung, Technologie und Raumfahrt | - |
Appears in Collections: | Publications with full text |
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File | Description | Size | Format | |
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Airport2030_PRE_FinalPresentation_Airbus_2014-06-05.pdf | 58.5 MB | Adobe PDF | View/Open |
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