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.
Research on Aerodynamic Shape Design of Wings of Hypersonic Aircrafts
Advances in Engineering res
International Conference on Mechanics, Electronics Engineering and Automation ; 2024 July 26, 2024 - July 28, 2024
Proceedings of the 2024 International Conference on Mechanics, Electronics Engineering and Automation (ICMEEA 2024) ; Kapitel : 9 ; 75-85
24.09.2024
11 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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