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. Preprints2024, 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
Dunmoye, G. Computational Analysis of Various Winglet Design Types on a Boeing 737 Aircraft. Preprints2024, 2024012000. https://doi.org/10.20944/preprints202401.2000.v1
APA Style
Dunmoye, G. (2024). Computational Analysis of Various Winglet Design Types on a Boeing 737 Aircraft. Preprints. https://doi.org/10.20944/preprints202401.2000.v1
Chicago/Turabian Style
Dunmoye, G. 2024 "Computational Analysis of Various Winglet Design Types on a Boeing 737 Aircraft" Preprints. 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
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.