Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 14, 30 November 2023


Open Access | Article

Study on application of winglets in drones

Jiajun Li * 1
1 Sun Yat-sen University

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 14, 108-111
Published 30 November 2023. © 2023 The Author(s). Published by EWA Publishing
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Citation Jiajun Li. Study on application of winglets in drones. TNS (2023) Vol. 14: 108-111. DOI: 10.54254/2753-8818/14/20240906.

Abstract

With the rapid development of drone technology, methods to improve drone performance have emerged endlessly. Reducing air resistance can significantly improve drones’ fight performance. The winglet is used to control the turbulence and vortices. The widespread application of winglets in the field of military and civil aviation has enabled winglets to be applied to drones to improve flight range and economic efficiency. As different winglets have different impacts on drones’ flight performance, this article focuses on the influence of different winglets on enhancing lift and reducing resistance of small civilian drones. In detail, three representative winglets are taken as the specific research objects, including the fusion winglet, the double fork scimitar winglets, and wingtip fence. The aerodynamic characteristics and the structural designs are comprehensively introduced. The importance of winglets in improving aircraft performance, energy saving and environmental protection is briefly explained. This article may offer a reference for the design of drones.

Keywords

Induced Drag, Winglet, Drone

References

1. Lu Honglei, Liu Tiejun, Ma Tuliang, et al. Analysis of aerodynamic characteristics of modern advanced winglets. Scientific and technological information, 2013, 18: 375-376.

2. Luo Yue. Study on lifting resistance characteristics and parameter optimization of fusion winglets. Nanchang Hangkong University, 2023.

3. Ma Yumin, Wei Jianlong. Study on drag reduction effects of fusion winglets. Advances in Aeronautical Engineering, 2018, 9(2): 7.

4. Wang Dan, Tao Yujin, Li Peifeng, et al. Application of different types of winglets in drone design. Journal of Naval Aeronautical Engineering, 2017, 32(5): 7.

5. Li Yufei, Bai Junqiang, Guo Bozhi, et al. Design and study of civil transport aircraft wing-tip devices based on FFD technology. Journal of Northwestern Polytechnical University, 2015, 33(4): 7.

6. Qi Mengka, Chen Mingyan. Study of flow fields near the tip of the wing and drag reduction mechanism of sails. Hydrodynamic experiments and measurements, 1995, 9(1): 38-45.

7. Zheng Benwu, Chen Mingyan. Optimized design of wingtip fence blades. Journal of Aerodynamics, 1995,013 (1): 105-109

8. TRIMBLE S. Low-price fuel drag. Flight International, 2016, 189(29):28-29.

9. Ding Songbin, Fan Jiafeng, Ma Tengyu. Economic analysis of A-type aircraft modified winglets based on cost benefit theory. Progress in aeronautical engineering, 2021,12 (02): 106-111+121.

10. Jiang Yongquan. The Design of Airplane Winglet. Aeronautical Industry Press, 2009:19-20.

Data Availability

The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.

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Volume Title
Proceedings of the 3rd International Conference on Computing Innovation and Applied Physics
ISBN (Print)
978-1-83558-191-9
ISBN (Online)
978-1-83558-192-6
Published Date
30 November 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/14/20240906
Copyright
30 November 2023
Open Access
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited

Copyright © 2023 EWA Publishing. Unless Otherwise Stated