Research on Aerodynamic Shape Design of Wings of Hypersonic Aircrafts

DOI

10.2991/978-94-6463-518-8_9How to use a DOI?

Keywords

Hypersonic vehicle; Aerodynamic; Profile design

Abstract

One of the primary fields of aerospace study is aerodynamic profile design. Most of the current research focuses on the design of subsonic aircraft, but there is a gap in hypersonic aircraft. As a result, the aerodynamic configuration of hypersonic vehicles is the subject of this paper. The researchers discovered the foundation, trend, and expansion of the current aerodynamic configuration research of each part by introducing the aerodynamic optimization methods of the four airplane parts. The research results show that multi-scientific collaborative design utilizing numerical methodologies and the integration approach of individual component designs is required for the fuselage. While the wing portion can raise the aircraft’s development quality through optimization design simulation, the “blunt head” of the bow can still be optimized to increase safety and save costs. The wing component can enhance the calibre of aircraft development using design simulation and optimization. Therefore, the design of hypersonic vehicles relies on precise and effective algorithms and numerical models. The purpose of this study is to explore and fill the gap in the hypersonic aerodynamic design of aircraft, to optimize the design scheme under the condition of low cost and high efficiency.

Copyright

© 2024 The Author(s)

Open Access

Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

Download article (PDF)

TY  - CONF
AU  - Rui Du
AU  - Wenjie Qi
AU  - Zihan Yin
AU  - Yitong Zhang
PY  - 2024
DA  - 2024/09/28
TI  - Research on Aerodynamic Shape Design of Wings of Hypersonic Aircrafts
BT  - Proceedings of the 2024 International Conference on Mechanics, Electronics Engineering and Automation (ICMEEA 2024)
PB  - Atlantis Press
SP  - 75
EP  - 85
SN  - 2352-5401
UR  - https://doi.org/10.2991/978-94-6463-518-8_9
DO  - 10.2991/978-94-6463-518-8_9
ID  - Du2024
ER  -