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Application of FDM technology to reduce aerodynamic drag

Alberto Sanchez Ramirez (Escuela Técnica Superior de Ingeniería Aeronáutica y del Espacio ETSIAE, Polytechnic University of Madrid, Madrid, Spain)
Manuel Enrique Islán Marcos (Ingeniería Mecánica, Química y Diseño Industrial, Polytechnic University of Madrid, Madrid, Spain)
Fernando Blaya Haro (Ingeniería Mecánica, Química y Diseño Industrial, Polytechnic University of Madrid, Madrid, Spain)
Roberto D’Amato (Ingeniería Mecánica, Química y Diseño Industrial, Polytechnic University of Madrid, Madrid, Spain)
Rodolfo Sant (Escuela Técnica Superior de Ingeniería Aeronáutica y del Espacio ETSIAE, Polytechnic University of Madrid, Madrid, Spain)
José Porras (Escuela Tecnica Superior de Ingenieria, Universidad Pontificia Comillas Escuela Tecnica Superior de Ingenieria, Madrid, Spain)

Rapid Prototyping Journal

ISSN: 1355-2546

Article publication date: 31 May 2019

Issue publication date: 12 July 2019

318

Abstract

Purpose

The purpose of this paper is to analyze the aerodynamic improvements obtained in a wing section with a NACA 0018 airfoil manufactured using the fused deposition modeling (FDM) technique with regard to a smooth surface made by milling. The creation of micro-riblets on the surface of the airfoil, due to the deposition of the material layer by layer, improves the general aerodynamic performance of the parts, provided that the riblets are parallel to the flow line. The incidence of the thickness of the thread deposited in each layer – to be the variable on which the geometry of the riblets is based – was studied.

Design/methodology/approach

The wing section was designed using 3D software. Three different models were designed by rapid prototyping, using additive and subtractive manufacturing. Two of the profiles were manufactured using FDM varying the thickness of the layer to be able to compare the aerodynamic improvements. The third model was manufactured using a subtractive rapid prototyping machine generating a smooth surface profile. These three models were tested inside the wind tunnel to be able to quantify the aerodynamic efficiency according to the geometry and the riblets size.

Findings

The manufacture of an aerodynamic profile using FDM provides, in addition to the lightness and the ability to design parts with complex geometries, an improvement in the aerodynamic efficiency of 10 per cent compared with profiles with a smooth surface.

Practical implications

With the aerodynamic advantage gained through the use of FDM positions, the additive manufacturing serves as an excellent alternative for the manufacture of lightweight aerodynamic parts, with low structural loading and with low Reynolds number (∼5·105). This technological advantage would be applied to the UAV (unmanned aerial vehicle) industry.

Originality/value

The study carried out in this article demonstrates that the use of FDM as a manufacture process of end-used parts that are subject to movement generates an additional advantage that had not been considered. The additive manufacturing allows us to directly manufacture riblets by creating the necessary surface so as to reduce the aerodynamic drag.

Keywords

Citation

Sanchez Ramirez, A., Islán Marcos, M.E., Blaya Haro, F., D’Amato, R., Sant, R. and Porras, J. (2019), "Application of FDM technology to reduce aerodynamic drag", Rapid Prototyping Journal, Vol. 25 No. 4, pp. 781-791. https://doi.org/10.1108/RPJ-09-2018-0251

Publisher

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Emerald Publishing Limited

Copyright © 2019, Emerald Publishing Limited

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