DC FieldValueLanguage
dc.contributor.advisorScholz, Dieter-
dc.contributor.authorDesenfans, Philip-
dc.date.accessioned2022-07-18T08:34:07Z-
dc.date.available2022-07-18T08:34:07Z-
dc.date.issued2019-06-01-
dc.identifier.urihttp://hdl.handle.net/20.500.12738/13152-
dc.description.abstractPurpose - The paper presents a theoretical framework that describes the aerodynamics of a falling maple (Acer pseudoplatanus) seed. --- Methodology - A semi-empirical method is developed that provides a ratio stating how much longer a seed falls in air compared to freefall. The generated lift is calculated by evaluating the integral of two-dimensional airfoil elements using a preliminary falling speed. This allows for the calculation of the definitive falling speed using Blade Element Momentum Theory (BEMT); hereafter, the fall duration in air and in freefall are obtained. Furthermore, the input-variables of the calculation of lift are transformed to require only the length and width of the maple seed. Lastly, the method is applied to two calculation examples as a means of validation. --- Findings - The two example calculations gave percentual errors of 5.5% and 3.7% for the falling speed when compared to measured values. The averaged result is that a maple seed falls 9.9 times longer in air when released from 20 m; however, this result is highly dependent on geometrical parameters which can be accounted for using the constructed method. --- Research limitations - Firstly, the coefficient of lift is unknown for the shape of a maple seed. Secondly, the approximated transient state is yet to be verified by measurement. --- Originality / Value - The added value of this report lies in the reduction of simplifications compared to BEMT approaches. In this way a large amount of accuracy is achieved due to the inclusion of many geometrical parameters, even though simplicity is maintained. This has been accomplished through constructing a simple three-step method that is fundamental and essentially non-iterative.en_US
dc.language.isoen_USen_US
dc.publisherAircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciencesen_US
dc.rights.urihttps://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.subjectAerodynamiken_US
dc.subjectAhornen_US
dc.subjectAuftrieben_US
dc.subjectStrömungsabrissen_US
dc.subjectAerodynamisches Profilen_US
dc.subjectAnstellwinkelen_US
dc.subjectFreier Fallen_US
dc.subjectBergahornen_US
dc.subjectSamenen_US
dc.subjectEvolutionsbiologieen_US
dc.subjectAerodynamicsen_US
dc.subjectMapleen_US
dc.subjectLift (Aerodynamics)en_US
dc.subjectStalling (Aerodynamics)en_US
dc.subjectAerofoilsen_US
dc.subjectAngle of attack (Aerodynamics)en_US
dc.subjectAcer pseudoplatanusen_US
dc.subjectSeedsen_US
dc.subjectEvolution (Biology)en_US
dc.subjectBlade Element Momentum Theoryen_US
dc.subjectBEMTen_US
dc.subjectfree fallen_US
dc.subjectpost-stallen_US
dc.subjectautorotationen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleThe Aerodynamics of a Falling Maple Seeden_US
dc.typeStudyThesisen_US
openaire.rightsinfo:eu-repo/semantics/openAccessen_US
tuhh.identifier.urnurn:nbn:de:gbv:18302-reposit-148425-
tuhh.note.externTrueen_US
tuhh.oai.showtrueen_US
tuhh.publication.instituteForschungsgruppe Flugzeugentwurf und -systeme (AERO)en_US
tuhh.publication.instituteDepartment Fahrzeugtechnik und Flugzeugbauen_US
tuhh.publication.instituteFakultät Technik und Informatiken_US
tuhh.publisher.doi10.15488/9373-
tuhh.publisher.urlhttps://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2019-06-01.016-
tuhh.publisher.urlhttps://n2t.net/ark:/13960/t4fn9pt5b-
tuhh.type.opusStudienarbeit-
dc.type.casraiOther-
dc.type.diniStudyThesis-
dc.type.driverother-
dcterms.DCMITypeText-
item.creatorGNDDesenfans, Philip-
item.openairetypeStudyThesis-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.creatorOrcidDesenfans, Philip-
item.languageiso639-1en_US-
item.grantfulltextopen-
item.cerifentitytypePublications-
item.advisorGNDScholz, Dieter-
item.fulltextWith Fulltext-
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