Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 18, 08 December 2023


Open Access | Article

Design of a new sweptback wing for a future supersonic aircraft—Research on lift drag characteristics and aerodynamic analysis

Lixin Xu * 1
1 Tongji University

* Author to whom correspondence should be addressed.

Advances in Humanities Research, Vol. 18, 1-9
Published 08 December 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 Lixin Xu. Design of a new sweptback wing for a future supersonic aircraft—Research on lift drag characteristics and aerodynamic analysis. TNS (2023) Vol. 18: 1-9. DOI: 10.54254/2753-8818/18/20230256.

Abstract

In recent years, with the gradual development of the aviation industry, how to make supersonic aircraft truly used in military air defense has become a global problem. In this paper, the wing design of supersonic aircraft is studied, a swept back symmetrical wing suitable for supersonic reconnaissance aircraft is designed with reasonable aspect ratio, span length, sweep angle, thrust weight ratio and wing load. On the basis of the aerodynamic characteristics of the aircraft analyzed, the inboard electron, outboard electron, flasheron, leading edge flap and all moving tip are designed to ensure the controllability in the flight line and to maintain the balance and stability of the aircraft. The qualitative analysis of the flight performance of the wing is also performed. This paper provides a possibility for the design of supersonic aircraft in the future.

Keywords

supersonic, wing, lift, drag, aviation

References

1. Abdullah Nur Azam; Sulaeman Erwin. Aeroelastic Tailoring of Oscillating Supersonic Wing with External Stores [J]. Applied Mechanics and Materials, 2013.

2. Zhonglai Wang, Xiaorong Hu, Yingdong Wu. Energy-efficient wing design for flapping wing micro aerial vehicles [J]. Journal of Mechanical Science and Technology, 2019.

3. Z. Siddiqi, J.W. Lee. A computational fluid dynamics investigation of subsonic wing designs for unmanned aerial vehicle application [J]. Proceedings of the Institution of Mechanical Engineers, 2019.

4. Binder Simon, Wildschek Andreas, De Breuker Roeland. The interaction between active aeroelastic control and structural tailoring in aeroservoelastic wing design [J]. Aerospace Science and Technology, 2021.

5. M. Nazmul Haque; Mohammad Ali; Ismat Ara. Experimental Investigation on the Performance of NACA 4412 Aerofoil with Curved Leading Edge Planform [J]. Procedia Engineering, 2015.

6. Faber Y. Silitonga, M. Agoes Moelyadi. Comparative Study of Wing Lift Distribution Analysis for High Altitude Long Endurance (HALE) Unmaned Aerial Vehicle [J]. Journal of Physics: Conference Series, 2018.

7. Lei Yao; Wenjie Yang; Yiyong Huang. Aerodynamic performance of distributed electric propulsion with wing interaction [J]. Journal of Zhejiang University-SCIENCE A, 2022.

8. G. K. Morikawa; T. F. Coleman. On Supersonic Wing-Body Center of Pressure [J]. Journal of the Aeronautical Sciences, 2012.

9. Kale S; Pendharkar E. Effects of wing twist on lift and drag characteristics of blended wing body aircraft [J]. Journal of Physics: Conference Series, 2021.

10. Sabri Farhad, Elzaabalawy Assem, Meguid. Aeroelastic behaviour of a flexible morphing wing design for unmanned aerial vehicle [J]. Acta Mechanica, 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
ISBN (Print)
978-1-83558-201-5
ISBN (Online)
978-1-83558-202-2
Published Date
08 December 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/18/20230256
Copyright
© 2023 The Author(s)
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