License: CC BY-NC-SA 4.0 (Attribution-NonCommercial-ShareAlike) CC BY-NC-SA 4.0 (Attribution-NonCommercial-ShareAlike)
Publisher URL: https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2019-06-01.016
https://n2t.net/ark:/13960/t4fn9pt5b
Publisher DOI: 10.15488/9373
Title: The Aerodynamics of a Falling Maple Seed
Language: 
Authors: Desenfans, Philip 
Keywords: Aerodynamik; Ahorn; Auftrieb; Strömungsabriss; Aerodynamisches Profil; Anstellwinkel; Freier Fall; Bergahorn; Samen; Evolutionsbiologie; Aerodynamics; Maple; Lift (Aerodynamics); Stalling (Aerodynamics); Aerofoils; Angle of attack (Aerodynamics); Acer pseudoplatanus; Seeds; Evolution (Biology); Blade Element Momentum Theory; BEMT; free fall; post-stall; autorotation
Issue Date: 1-Jun-2019
Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences
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 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.
URI: http://hdl.handle.net/20.500.12738/13152
Institute: Forschungsgruppe Flugzeugentwurf und -systeme (AERO) 
Department Fahrzeugtechnik und Flugzeugbau 
Fakultät Technik und Informatik 
Type: Study Thesis
Advisor: Scholz, Dieter  
Appears in Collections:SAIL

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