DC ElementWertSprache
dc.contributor.authorScholz, Dieter-
dc.contributor.authorBudziak, Kinga-
dc.contributor.authorMariën, Floris-
dc.date.accessioned2026-09-25T11:22:28Z-
dc.date.available2026-09-25T11:22:28Z-
dc.date.issued2026-09-08-
dc.identifier.urihttps://hdl.handle.net/20.500.12738/20140-
dc.description.abstractBackground – Induced drag is calculated from C_D,i = C_L²/(pi*A*e). Clearly, induced drag can be reduced by increasing the aspect ratio, A. For elliptical wings, e = 1. Tapered wings have e < 1, even at best taper ratio, lambda = c_t/c_r of 0.45 (NASA Report 921) respectively 0.357 (Hoerner 1965). With Hoerner's f(lambda) it is possible to calculate e = 1/(1+f(lambda)*A). More is possible. --- Purpose – Calculate span efficiency factors (e) of straight (unswept) wings for various aspect ratios (A) and taper ratios (0 < lambda < 1) using computational fluid dynamics (CFD). Use the notation from Hoerner. From CFD results calculate e and continue to calculate f(lambda) = (1-e)/(A*e). Users of the results can calculate back to the span efficiency factor with e = 1/(1+f(lambda)*A). --- Methodology – Wings are modeled in AVL and VSPAERO with VLM and Panel Method (NACA 0010) with different aspect ratios and taper ratios. At a selected angle of attack, the lift coefficient and the induced drag coefficient are calculated. From the CFD results the span efficiency factor, e and f(lambda) are calculated. f(lambda) is plotted in comparison to Hoerner's (theoretical) curve. --- Findings – Span efficiency factor, e decreases with increasing aspect ratio, A. The panel method from VSPAERO shows curves approaching Hoerner's curve with increasing aspect ratio. Calculated values of f(lamda) are larger resulting in lower span efficiency factor (e). The Vortex Lattice Method (VLM) offered by AVL also shows curves approaching Hoerner's curve with increasing aspect ratio. However, calculated values of f(lamda) are smaller resulting in a larger span efficiency factor (e). The VLM of VSPAERO shows curves f(lamda) of similar magnitude as Hoerner, but without clear tendencies. Shown is only the result for A = 10. --- Practical Implications – Hoerner's curve seems to be a helpful and simple means to calculate the span efficiency factor (e). To assume that f(lambda) is independent of aspect ratio may be a simplification. A hypothesis is that Hoerner's curve represents values for an aspect ratio approaching infinity. --- Originality – Results calculated with AVL were published by Budziak (2015) and with VSPAERO by Mariën (2021), both supervised by Scholz. This is the first presentation at a conference.en
dc.language.isoenen_US
dc.subjectLuftfahrten_US
dc.subjectLuftfahrzeugen_US
dc.subjectFlugzeugaerodynamiken_US
dc.subjectLuftwiderstanden_US
dc.subjectAeronauticsen_US
dc.subjectAirplanesen_US
dc.subjectAerodynamicsen_US
dc.subjectComputational Fluid Dynamicsen_US
dc.subjectFlugzeugen_US
dc.subjectNumerische Strömungssimulationen_US
dc.subjectCFDen_US
dc.subjectPanelverfahrenen_US
dc.subjectTabellenkalkulationen_US
dc.subjectWirbelgitterverfahrenen_US
dc.subjectDrag (Aerodynamics)en_US
dc.subjectElectronic spreadsheetsen_US
dc.subjectVLMen_US
dc.subjectdragen_US
dc.subjectinduceden_US
dc.subjectOswalden_US
dc.subjectfactoren_US
dc.subjectaircraften_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleInduced drag calculation of tapered wings - revisiting Hoerner's approach with AVL and VSPAEROen
dc.typePosteren_US
dc.relation.conferenceDeutscher Luft- und Raumfahrtkongress 2026en_US
dc.identifier.doi10.48441/4427.3781-
dc.description.versionNonPeerRevieweden_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-246357-
tuhh.oai.showtrueen_US
tuhh.publication.instituteForschungsgruppe Flugzeugentwurf und -systeme (AERO)en_US
tuhh.publication.instituteFakultät Luftfahrt- und Fahrzeugsystemeen_US
tuhh.type.opusPoster-
tuhh.type.rdmtrue-
dc.rights.cchttps://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.type.casraiConference Poster-
dc.type.diniOther-
dc.type.driverother-
dc.type.statusinfo:eu-repo/semantics/publishedVersionen_US
dcterms.DCMITypeImage-
datacite.relation.IsDocumentedByhttps://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2015-09-20.015-
datacite.relation.IsDocumentedByhttps://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2021-07-16.018-
datacite.relation.IsSupplementedBydoi:10.7910/DVN/0S1R14en_US
local.comment.externalSCHOLZ, Dieter, BUDZIAK, Kinga, MARIËN, Floris, 2026. Induced Drag Calculation of Tapered Wings – Revisiting Hoerner's Approach with Athena Vortex Lattice (AVL) and VSPAERO. Poster. German Aerospace Congress (Aachen, Germany, 08.-10.09.2026). Available from: https://doi.org/10.48441/4427.3781en_US
tuhh.apc.statusfalseen_US
item.cerifentitytypePublications-
item.creatorGNDScholz, Dieter-
item.creatorGNDBudziak, Kinga-
item.creatorGNDMariën, Floris-
item.languageiso639-1en-
item.fulltextWith Fulltext-
item.grantfulltextopen-
item.openairecristypehttp://purl.org/coar/resource_type/c_6670-
item.openairetypePoster-
item.creatorOrcidScholz, Dieter-
item.creatorOrcidBudziak, Kinga-
item.creatorOrcidMariën, Floris-
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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