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dc.identifier.uri http://dx.doi.org/10.15488/9373
dc.identifier.uri https://www.repo.uni-hannover.de/handle/123456789/9427
dc.contributor.advisor Scholz, Dieter DE
dc.contributor.author Desenfans, Philip ger
dc.date.accessioned 2020-02-17T11:05:03Z
dc.date.issued 2019
dc.identifier.citation Desenfans, Philip: Aerodynamics of the Maple Seed. Project. Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2019. URN: https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2019-06-01.016 ger
dc.description.abstract Purpose - 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 geo-metrical 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 essen-tially non-iterative. ger
dc.language.iso eng ger
dc.publisher Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences
dc.rights CC BY-NC-SA 4.0 Unported ger
dc.rights.uri https://creativecommons.org/licenses/by-nc-sa/4.0 ger
dc.subject Blade Element Momentum Theory eng
dc.subject BEMT eng
dc.subject free fall eng
dc.subject post-stall eng
dc.subject chord eng
dc.subject twist eng
dc.subject camber eng
dc.subject autorotation eng
dc.subject.classification Aerodynamik ger
dc.subject.classification Ahorn ger
dc.subject.classification Auftrieb ger
dc.subject.classification Strömungsabriss ger
dc.subject.classification Aerodynamisches Profil ger
dc.subject.classification Anstellwinkel ger
dc.subject.classification Freier Fall ger
dc.subject.classification Bergahorn ger
dc.subject.classification Samen ger
dc.subject.classification Evolutionsbiologie ger
dc.subject.ddc 600 | Technik ger
dc.subject.ddc 620 | Ingenieurwissenschaften und Maschinenbau ger
dc.subject.ddc 629,1 | Luft- und Raumfahrttechnik ger
dc.subject.lcsh Aerodynamics eng
dc.subject.lcsh Maple eng
dc.subject.lcsh Lift (Aerodynamics) eng
dc.subject.lcsh Stalling (Aerodynamics) eng
dc.subject.lcsh Aerofoils eng
dc.subject.lcsh Angle of attack (Aerodynamics) eng
dc.subject.lcsh Acer pseudoplatanus eng
dc.subject.lcsh Seeds eng
dc.subject.lcsh Evolution (Biology) eng
dc.title Aerodynamics of the Maple Seed eng
dc.type Book ger
dc.type Text ger
dc.relation.urn https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2019-06-01.016
dc.relation.other https://n2t.net/ark:/13960/t4fn9pt5b
dc.description.version publishedVersion ger
tib.accessRights frei zug�nglich ger


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