Wide-speed-range hypersonic vehicle aerodynamic configuration: research progress and future challenges

CUI Kai; CHANG Siyuan; XIAO Yao; LI Guangli; TIAN Zhongwei

doi:10.6052/1000-0992-26-009

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Article Navigation > Advances in Mechanics > 2026 > Accepted Manuscript

Cui K, Chang S Y, Xiao Y, Li G L, Tian Z W. Wide-speed-range hypersonic vehicle aerodynamic configuration: research progress and future challenges. Advances in Mechanics, in press doi: 10.6052/1000-0992-26-009

Citation:

Cui K, Chang S Y, Xiao Y, Li G L, Tian Z W. Wide-speed-range hypersonic vehicle aerodynamic configuration: research progress and future challenges. Advances in Mechanics, in press doi: 10.6052/1000-0992-26-009

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Wide-speed-range hypersonic vehicle aerodynamic configuration: research progress and future challenges

doi: 10.6052/1000-0992-26-009 cstr: 32046.14.1000-0992-26-009

CUI Kai^{1, 2},
CHANG Siyuan^{1
,
,},
XIAO Yao¹,
LI Guangli^{1, 2},
TIAN Zhongwei¹

1.
Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
2.
School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China

More Information

Corresponding author: changsiyuan@imech.ac.cn
Received Date: 2026-02-28
Accepted Date: 2026-05-27

Available Online: 2026-05-30

Abstract

Abstract

Wide-speed-range hypersonic vehicles, characterized by their capabilities for horizontal takeoff and landing, reusability, and flight across vast airspace, are expected to serve as the core platforms for future space round-trip and rapid long-distance delivery missions. The aerodynamic configuration design of these vehicles directly determines their overall performance and technical feasibility, while also confronting multiple fundamental theoretical and engineering challenges, such as multi-physics field coupling and adaptation to a wide speed range. This paper systematically reviews the research progress on aerodynamic configurations in this field, both domestically and internationally. Firstly, it reviews the evolutionary trajectory of typical foreign development projects and conceptual schemes, highlighting that aerodynamic configuration design has shifted from optimizing performance for a single speed regime to a comprehensive trade-off across the entire flight envelope. Subsequently, the current research status of fixed configurations is summarized from four aspects: waveriders, high-pressure capturing wings, bidirectional flying wings, and optimization design for wide-speed-range aerodynamic configurations. Furthermore, the development of morphing technologies is reviewed, and the primary morphing strategies applicable to wide-speed-range hypersonic flight are synthesized. Finally, an in-depth analysis of the core challenges currently facing the design of wide-speed-range hypersonic aerodynamic configurations is conducted at the levels of aerodynamic design, multidisciplinary coupling design, and application. Corresponding future development suggestions are proposed, aiming to provide a reference for research and engineering practice in related fields.
- wide-speed-range,
- hypersonic,
- aerodynamic configuration,
- morphing,
- waverider,
- high-pressure capturing wing

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References(173)

References

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