Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 9, 13 November 2023


Open Access | Article

The performance and application of sweep wing aircraft

Kainan Chen * 1
1 University of Shanghai for Science and Technology

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 9, 73-80
Published 13 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 Kainan Chen. The performance and application of sweep wing aircraft. TNS (2023) Vol. 9: 73-80. DOI: 10.54254/2753-8818/9/20240719.

Abstract

With the development of science and technology, more and more civil and military aircraft have adopted swept-back wing shapes. this paper explores the relationship between the angle of swept-wing and the lift, drag and lift-drag ratio of the aircraft, and expounds it in combination with the actual swept-wing aircraft, such as Boeing737 and MIG-23 to find the best sweep angle of the aircraft in the appropriate range and analyze the effect of swept wing angle on flight speed. This paper studies and analyzes the data through literature retrieval and data processing and cites data models from many academic journals. The experimental data are mainly derived from computational fluid dynamics and wind tunnel simulation. This paper finds that a wider sweep angle can result in better aerodynamic performance, suited for supersonic flight, while a smaller sweep angle can result in a better lift-drag ratio, it is suitable for takeoff and landing of aircraft and low-speed flight attitude.

Keywords

Sweep Wing, Lift-Drag Ratio, Aerodynamics

References

1. Sheng Zihao, Fan Geng & Hantian. (2022). Optimal sweep Angle prediction model of variable sweep wing with single velocity based on CFD. Journal of Naval Aeronautical University (01),153-158.

2. Huang Z F, Lu X Z & Yu G C. (2014). Crossflow stability analysis and transition prediction of wing boundary layer. Journal of Aerodynamics (01),14-20.

3. Lifang ZENG, Liu LIU, Xueming SHAO, Jun LI. (2023) Mechanism analysis of hysteretic aerodynamic characteristics on variable-sweep wings. Chinese Journal of Aeronautics, 212-222.

4. Lance W. Traub, Samarth M. Chandrashekar. (2016) Experimental study on the effects of wing sweep on Gurney flap performance, Aerospace Science and Technology, Pages 57-63, ISSN 1270-9638.

5. Pei Dai, Binbin Yan, Wei Huang, Yifei Zhen, Mingang Wang, Shuangxi Liu. (2020) Design and aerodynamic performance analysis of a variable-sweep-wing morphing waverider, Aerospace Science and Technology, 105703, ISSN 1270-9638.

6. U. Goldberg, (2005) Hypersonic turbulent flow predictions using CFD++, in: AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference

7. Li Aijun, Shen Yi, Zhang Weiguo.(2002). A fuzzy control method for high elevation flight of aircraft. Aircraft Design (04),42-44. doi:10.19555/j.cnki.1673-4599

8. Zuo Yuhan, Yang Yong, Li Dong, et al. (2010) Experimental study on the cross-flow instability of swept-back wing Boundary Layer [J]. Journal of Aerodynamics,28 (5):495-502.

9. Wang F C. (1994). Review of design characteristics of MIG-23 aircraft. Aircraft Design (02),72-80. doi:10.19555/j.cnki.1673-4599.1994.02.014.

Data Availability

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

This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License. Authors who publish this series agree to the following terms:

1. Authors retain copyright and grant the series right of first publication with the work simultaneously licensed under a Creative Commons Attribution License that allows others to share the work with an acknowledgment of the work's authorship and initial publication in this series.

2. Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the series's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgment of its initial publication in this series.

3. Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See Open Access Instruction).

Volume Title
Proceedings of the 3rd International Conference on Computing Innovation and Applied Physics
ISBN (Print)
978-1-83558-129-2
ISBN (Online)
978-1-83558-130-8
Published Date
13 November 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/9/20240719
Copyright
13 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