Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 5, 25 May 2023


Open Access | Article

Research on the Principle of Aircraft Take-off and the Functions of Its Parts

Chenhao Zhu * 1
1 School of International Education, Dalian Jiaotong University, Dalian, Liaoning Province, China,116028

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 5, 299-304
Published 25 May 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 Chenhao Zhu. Research on the Principle of Aircraft Take-off and the Functions of Its Parts. TNS (2023) Vol. 5: 299-304. DOI: 10.54254/2753-8818/5/20230534.

Abstract

Aeroplane-One of the greatest inventions of the twentieth century. Since ancient times, man has dreamed of flying in the sky like a bird. In modern society, due to the rapid development of science and technology (fluid mechanics, automatic control system, etc.), aircraft has become a basic means of transportation. This paper mainly studies how the aircraft takes off and the role of its individual components. Through the method of literature reading and analysis, the force of aircraft takeoff, as well as the role of wings and flaps (Kruger flaps, slit flaps, fuller flaps) in the take-off process are summarized.According to Bernoulli's principle, the lift of an aircraft is mainly generated by the wings, and parts such as flaps are used to regulate the flight state of the aircraft. At the same time, the aircraft must overcome a variety of drags during flight, including frictional resistance, tip resistance and induced resistance.

Keywords

fluid dynamics, wings, flaps, aircraft, induced drag, interference resistance.

References

1. Bi Xiaolin, "Bernoulli's principle and its applications," Secondary School Physics Teaching Reference, pp. 1-3, 3 2020

2. Shan Yongfei and Liu Linhai, "The Effect of Wing Plane Shape on Structural Weight of a Domestic Pre-developed Aircraft," 15 March 2001. Available:https://kns.cnki.net/kcms/detail/detail.aspx?dbcode=CJFD&dbname=CJFD2001&filename=MYFJ200101001&uniplatform=NZKPT&v=antxNfs_HaUTsM-93a_ YSAqCy8Pf8ijeFU-GVA_HAujE2USUGWRmeWKHDdWY7BEi.

3. BB senior, "Zhihu," Zhihu, Available: https://zhuanlan.zhihu.com/p/402446480. [Date of visit: 22 November 2022]

4. Wei Wei, Yuanqing Zhang, Rui He, Weijun Cui, "Research on Trailing Edge Flaps Motion Design of Large Civil Aircraft," Science and Technology Vision, 9 2018

5. Zhang Minghui, Chen Zhenli, Mao Jun, Wang Gang, Tan Zhaoguang, Wang Long, Zhang Binqian, "Wing-body fusion layout civil aircraft Kruger flap design," Aeronautics and Astronautical Journal, pp. 1-3, 25 9 2019

6. Xuebo Yao, "Design Analysis of Leading Edge Slatted Wing Structure," 15 Dec 1996. Available:https://kns.cnki.net/kcms/detail/detail.aspx?dbcode=CJFD&dbname=CJFD9697&filename=MYFJ199604004&uniplatform=NZKPT&v=14-W7V4yAYEZoIOdVHphEuBsWDpYDfFRTEN_73NUSBIu8lDBc1uAyj1oLVSH5C5d.

7. Guo Ma, Chao Li, Zhenpeng Zhu, Ziyu Liu, Junwen Huang, Aoyun Zhang, "Measuring Air Using Hall Elements Based on Pendulum Experiments," University Physics Experiments, 26 Apr, 2022.

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 2nd International Conference on Computing Innovation and Applied Physics (CONF-CIAP 2023)
ISBN (Print)
978-1-915371-53-9
ISBN (Online)
978-1-915371-54-6
Published Date
25 May 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/5/20230534
Copyright
25 May 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