Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.438
Fulltext available Open Access https://creativecommons.org/licenses/by-nc-sa/4.0/
DC FieldValueLanguage
dc.contributor.authorScholz, Dieter-
dc.date.accessioned2022-03-10T13:34:24Z-
dc.date.available2022-03-10T13:34:24Z-
dc.date.issued2010-
dc.identifier.urihttp://hdl.handle.net/20.500.12738/12643-
dc.description.abstractThe Blended Wing Body (BWB) configuration has a potential to reduce weight, if a single shell design is applied (8% better). It has a better glide ratio, L/D (10% to 15% better). However, this was not apparent from the scale model AC20.30. There is a potential for a reduction in fuel consumption (mostly due to better L/D) and hence also a reduction in emissions. A reduction in noise can only be achieved with engines on top. Increase of airport capacity is possible, if an aircraft for more than 750 passengers is designed. The aircraft will probably not have problems with wake turbulence. Direct Operating Costs (DOC) will benefit mostly from the scale effect (larger aircraft). But: There are open certification issues. The BWB has an unstable configuration, ditching is not solved, rotation on take-off needs to be further investigated and landing gear integration is difficult.en
dc.language.isoenen_US
dc.subjectPreliminary Sizingen_US
dc.subjectAerodynamicsen_US
dc.subjectWind Tunnelen_US
dc.subjectFlight Mechanicsen_US
dc.subjectStructuresen_US
dc.subjectMass Predictionen_US
dc.subjectSystem Integrationen_US
dc.subjectGround Handlingen_US
dc.subjectEmergencyen_US
dc.subjectWake Turbulenceen_US
dc.subjectAir Transport Systemen_US
dc.subjectInterior Designen_US
dc.subjectBWBen_US
dc.subjectBlended Wing Bodyen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleThe blended wing body (BWB) aircraft configurationen
dc.title.alternativeDie Blended Wing Body (BWB) Flugzeugkonfigurationde
dc.typePresentationen_US
dc.relation.conferenceKolloquium : 75 Jahre Flugzeugbaustudium in Hamburg (1935 – 2010)en_US
dc.identifier.doi10.48441/4427.438-
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-125073-
tuhh.oai.showtrueen_US
tuhh.publication.instituteDepartment Fahrzeugtechnik und Flugzeugbauen_US
tuhh.publication.instituteFakultät Technik und Informatiken_US
tuhh.publication.instituteForschungsgruppe Flugzeugentwurf und -systeme (AERO)en_US
tuhh.publisher.urlhttps://www.fzt.haw-hamburg.de/pers/Scholz/paper/75Jahre_Flugzeugbaustudium_Fachkolloquium_10-06-04_BWB-Flugzeugkonfiguration.pdf-
tuhh.type.opusPräsentation-
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-
item.creatorGNDScholz, Dieter-
item.openairetypePresentation-
item.openairecristypehttp://purl.org/coar/resource_type/c_c94f-
item.creatorOrcidScholz, Dieter-
item.languageiso639-1en-
item.grantfulltextopen-
item.cerifentitytypePublications-
item.fulltextWith Fulltext-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.orcid0000-0002-8188-7269-
crisitem.author.parentorgFakultät Technik und Informatik-
Appears in Collections:Publications with full text
Files in This Item:
File Description SizeFormat
75Jahre_Flugzeugbaustudium_Fachkolloquium_10-06-04_BWB-Flugzeugkonfiguration.pdf6.96 MBAdobe PDFView/Open
Show simple item record

Page view(s)

276
checked on May 3, 2024

Download(s)

162
checked on May 3, 2024

Google ScholarTM

Check

HAW Katalog

Check

Note about this record

Export

This item is licensed under a Creative Commons License Creative Commons