Article
Version 1
Preserved in Portico This version is not peer-reviewed
Computational Analysis of Various Winglet Design Types on a Boeing 737 Aircraft
Version 1
: Received: 27 January 2024 / Approved: 29 January 2024 / Online: 29 January 2024 (08:47:52 CET)
How to cite: Dunmoye, G. Computational Analysis of Various Winglet Design Types on a Boeing 737 Aircraft. Preprints 2024, 2024012000. https://doi.org/10.20944/preprints202401.2000.v1 Dunmoye, G. Computational Analysis of Various Winglet Design Types on a Boeing 737 Aircraft. Preprints 2024, 2024012000. https://doi.org/10.20944/preprints202401.2000.v1
Abstract
This research focuses on the computational design and analysis of various winglet Design types on a Boeing 737 aircraft. The idea is to compare the efficiencies of various winglet design types on a Boeing 737 aircraft half wing span and the picking out the best winglet design in respect to the pressure generated at the wing-tip and the lift-to-drag ratio of each winglet designs. The coefficient of lift-drag ratio in this research contribute to the reduction of fuel consumption
Keywords
SOLIDWORKS; lift-to-drag ratio; winglet; wingtip devices; lift; drag; vortices; pressure; angle of attack
Subject
Engineering, Aerospace Engineering
Copyright: This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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