Please use this identifier to cite or link to this item:
https://doi.org/10.48441/4427.3163
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Scholz, Dieter | - |
| dc.date.accessioned | 2026-02-10T17:48:02Z | - |
| dc.date.available | 2026-02-10T17:48:02Z | - |
| dc.date.issued | 2026-01-15 | - |
| dc.identifier.uri | https://hdl.handle.net/20.500.12738/18731 | - |
| dc.description.abstract | Startup companies are convinced the Blended Wing Body (BWB) configuration will revolutionize flight and will use "up to 50% less fuel than today’s commercial jets" (www.jetzero.aero). The US-based companies are JetZero and Natilus. In December 2025, Outbound Aerospace had to shut down, running out of funding. In contrast: "Substantial fuel reduction cannot be expected for passenger aircraft" is the research result from a former HAW Hamburg project featuring a flying BWB demonstrator called AC20230 with a span of 3 m. The presentation guides the audience through the aeronautical disciplines and shows with real numbers and a few equations what to expect beyond unfounded promises and artist's impressions. However, a viable application could be a BWB tanker. Large parts of such an aircraft could remain unpressurized, and like the Northrop B2 bomber, the BWB offers low-observable (stealth) characteristics. Even more important: The U.S. Air Force needs a tanker replacement and has funds available. In 2023, the U.S. Air Force awarded a $235-million contract to JetZero to build a full-scale demonstrator by 2027 in partnership with Scaled Composites (Northrop Grumman). | en |
| dc.language.iso | en | en_US |
| dc.subject | aviation | en_US |
| dc.subject | airplane | en_US |
| dc.subject | air transport system | en_US |
| dc.subject | flying wing | en_US |
| dc.subject | hybrid flying wing | en_US |
| dc.subject | Blended Wing Body | en_US |
| dc.subject | BWB | en_US |
| dc.subject | Box Wing Aircraft | en_US |
| dc.subject | BWA | en_US |
| dc.subject | square-cube-law | en_US |
| dc.subject | preliminary sizing | en_US |
| dc.subject | aerodynamics | en_US |
| dc.subject | Computational Fluid Dynamics | en_US |
| dc.subject | CFD | en_US |
| dc.subject | flight mechanics | en_US |
| dc.subject | mass prediction | en_US |
| dc.subject | system integration | en_US |
| dc.subject | ground handling | en_US |
| dc.subject | emergency evacuation | en_US |
| dc.subject | fire suppression | en_US |
| dc.subject | wake turbulence | en_US |
| dc.subject | aerodrome | en_US |
| dc.subject | interior design | en_US |
| dc.subject | flight test | en_US |
| dc.subject | wind tunnel | en_US |
| dc.subject | stability | en_US |
| dc.subject | center of gravity | en_US |
| dc.subject | CG | en_US |
| dc.subject | ventilation | en_US |
| dc.subject | landing gear | en_US |
| dc.subject | cargo | en_US |
| dc.subject | ditching | en_US |
| dc.subject | Airbus | en_US |
| dc.subject | Boeing | en_US |
| dc.subject | VELA | en_US |
| dc.subject | AC20.30 | en_US |
| dc.subject | JetZero | en_US |
| dc.subject | Natilus | en_US |
| dc.subject | Outbound Aerospace | en_US |
| dc.subject.ddc | 620: Ingenieurwissenschaften | en_US |
| dc.title | New Blended Wing Body (BWB) aircraft – is 50% fuel reduction a credible claim? | en |
| dc.type | Presentation | en_US |
| dc.relation.conference | Hamburg Aerospace Lecture Series 2026 | en_US |
| dc.identifier.doi | 10.48441/4427.3163 | - |
| dc.description.version | NonPeerReviewed | en_US |
| openaire.rights | info:eu-repo/semantics/openAccess | en_US |
| tuhh.identifier.urn | urn:nbn:de:gbv:18302-reposit-230604 | - |
| tuhh.oai.show | true | en_US |
| tuhh.publication.institute | Forschungsgruppe Flugzeugentwurf und -systeme (AERO) | en_US |
| tuhh.publication.institute | Fakultät Luftfahrt- und Fahrzeugsysteme | en_US |
| tuhh.publisher.doi | 10.5281/zenodo.18377808 | - |
| tuhh.type.opus | Präsentation | - |
| tuhh.type.rdm | true | - |
| 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 | SCHOLZ, Dieter, 2026. New Blended Wing Body (BWB) Aircraft – Is 50% Fuel Reduction a Credible Claim? Hamburg Aerospace Lecture Series (DGLR, RAeS, VDI, ZAL, HAW Hamburg), Hamburg, Germany, 15.01.2026. – Available from: https://doi.org/10.48441/4427.3163 | en_US |
| tuhh.apc.status | false | en_US |
| item.creatorOrcid | Scholz, Dieter | - |
| item.grantfulltext | open | - |
| item.fulltext | With Fulltext | - |
| item.creatorGND | Scholz, Dieter | - |
| item.languageiso639-1 | en | - |
| item.openairecristype | http://purl.org/coar/resource_type/c_c94f | - |
| item.cerifentitytype | Publications | - |
| item.openairetype | Presentation | - |
| crisitem.author.dept | Department Fahrzeugtechnik und Flugzeugbau (ehemalig, aufgelöst 10.2025) | - |
| crisitem.author.orcid | 0000-0002-8188-7269 | - |
| crisitem.author.parentorg | Fakultät Technik und Informatik (ehemalig, aufgelöst 10.2025) | - |
| Appears in Collections: | Publications with full text | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| text_2026_01_15_NewBWB.pdf | 15.97 MB | Adobe PDF | View/Open |
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