Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.3163
DC FieldValueLanguage
dc.contributor.authorScholz, Dieter-
dc.date.accessioned2026-02-10T17:48:02Z-
dc.date.available2026-02-10T17:48:02Z-
dc.date.issued2026-01-15-
dc.identifier.urihttps://hdl.handle.net/20.500.12738/18731-
dc.description.abstractStartup 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.isoenen_US
dc.subjectaviationen_US
dc.subjectairplaneen_US
dc.subjectair transport systemen_US
dc.subjectflying wingen_US
dc.subjecthybrid flying wingen_US
dc.subjectBlended Wing Bodyen_US
dc.subjectBWBen_US
dc.subjectBox Wing Aircraften_US
dc.subjectBWAen_US
dc.subjectsquare-cube-lawen_US
dc.subjectpreliminary sizingen_US
dc.subjectaerodynamicsen_US
dc.subjectComputational Fluid Dynamicsen_US
dc.subjectCFDen_US
dc.subjectflight mechanicsen_US
dc.subjectmass predictionen_US
dc.subjectsystem integrationen_US
dc.subjectground handlingen_US
dc.subjectemergency evacuationen_US
dc.subjectfire suppressionen_US
dc.subjectwake turbulenceen_US
dc.subjectaerodromeen_US
dc.subjectinterior designen_US
dc.subjectflight testen_US
dc.subjectwind tunnelen_US
dc.subjectstabilityen_US
dc.subjectcenter of gravityen_US
dc.subjectCGen_US
dc.subjectventilationen_US
dc.subjectlanding gearen_US
dc.subjectcargoen_US
dc.subjectditchingen_US
dc.subjectAirbusen_US
dc.subjectBoeingen_US
dc.subjectVELAen_US
dc.subjectAC20.30en_US
dc.subjectJetZeroen_US
dc.subjectNatilusen_US
dc.subjectOutbound Aerospaceen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleNew Blended Wing Body (BWB) aircraft – is 50% fuel reduction a credible claim?en
dc.typePresentationen_US
dc.relation.conferenceHamburg Aerospace Lecture Series 2026en_US
dc.identifier.doi10.48441/4427.3163-
dc.description.versionNonPeerRevieweden_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-230604-
tuhh.oai.showtrueen_US
tuhh.publication.instituteForschungsgruppe Flugzeugentwurf und -systeme (AERO)en_US
tuhh.publication.instituteFakultät Luftfahrt- und Fahrzeugsystemeen_US
tuhh.publisher.doi10.5281/zenodo.18377808-
tuhh.type.opusPräsentation-
tuhh.type.rdmtrue-
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.externalSCHOLZ, 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/10.48441/4427.3163en_US
tuhh.apc.statusfalseen_US
item.openairetypePresentation-
item.creatorOrcidScholz, Dieter-
item.creatorGNDScholz, Dieter-
item.grantfulltextopen-
item.languageiso639-1en-
item.fulltextWith Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_c94f-
item.cerifentitytypePublications-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau (ehemalig, aufgelöst 10.2025)-
crisitem.author.orcid0000-0002-8188-7269-
crisitem.author.parentorgFakultät Technik und Informatik (ehemalig, aufgelöst 10.2025)-
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