Please use this identifier to cite or link to this item:
https://doi.org/10.48441/4427.2478
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Schiktanz, Daniel | - |
dc.contributor.author | Scholz, Dieter | - |
dc.date.accessioned | 2025-05-16T15:18:12Z | - |
dc.date.available | 2025-05-16T15:18:12Z | - |
dc.date.issued | 2011-12-21 | - |
dc.identifier.uri | https://hdl.handle.net/20.500.12738/17594 | - |
dc.description.abstract | This survey was prepared for having a structured compendium about the aerodynamic characteristics of several supercritical airfoils. It may be used within the scope of the design of commercial airliners. The survey is based on published data coming from wind tunnel tests performed at the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel. All of the referenced reports are published on the NASA Technical Reports Server (NTRS). | 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 | airliners | en_US |
dc.subject | commercial | en_US |
dc.subject | aircraft | en_US |
dc.subject | design | en_US |
dc.subject | wing | en_US |
dc.subject | airfoil | en_US |
dc.subject | catalog | en_US |
dc.subject | supercritical | en_US |
dc.subject | aerodynamics | en_US |
dc.subject | wind tunnel | en_US |
dc.subject | test | en_US |
dc.subject | NASA | en_US |
dc.subject | Langley | en_US |
dc.subject | transonic | en_US |
dc.subject | relative | en_US |
dc.subject | thickness | en_US |
dc.subject | lift | en_US |
dc.subject | coefficient | en_US |
dc.subject | Mach | en_US |
dc.subject | Reynolds | en_US |
dc.subject | number | en_US |
dc.subject.ddc | 620: Ingenieurwissenschaften | en_US |
dc.title | Survey of experimental data of selected supercritical airfoils | en |
dc.type | Report | en_US |
dc.identifier.doi | 10.48441/4427.2478 | - |
dc.description.version | NonPeerReviewed | en_US |
openaire.rights | info:eu-repo/semantics/openAccess | en_US |
tuhh.identifier.urn | urn:nbn:de:gbv:18302-reposit-212153 | - |
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_TN_Supercritical_Airfoils_11-12-21.pdf | - |
tuhh.type.opus | Report | - |
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 | Text | - |
local.comment.external | SCHIKTANZ, Daniel, SCHOLZ, Dieter, 2011. Survey of Experimental Data of Selected Supercritical Airfoils. Technical Note. Aircraft Design and Systems Group (AERO). Hamburg University of Applied Sciences (HAW Hamburg). Available from: https://doi.org/10.48441/4427.2478 | en_US |
tuhh.apc.status | false | en_US |
item.creatorGND | Schiktanz, Daniel | - |
item.creatorGND | Scholz, Dieter | - |
item.grantfulltext | open | - |
item.openairetype | Report | - |
item.fulltext | With Fulltext | - |
item.languageiso639-1 | en | - |
item.cerifentitytype | Publications | - |
item.creatorOrcid | Schiktanz, Daniel | - |
item.creatorOrcid | Scholz, Dieter | - |
item.openairecristype | http://purl.org/coar/resource_type/c_18cf | - |
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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Airport2030_TN_Supercritical_Airfoils_11-12-21.pdf | 12.71 MB | Adobe PDF | View/Open |
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