Integrated scheme of air-breathing high-speed aircraft: review and prospect

WANG Zhenguo; LIANG Jianhan; FAN Xiaoqiang; ZHAO Yuxin; WANG Yi; ZHAO Yilong; XIONG Bing

doi:10.7638/kqdlxxb-2023.0116

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Integrated scheme of air-breathing high-speed aircraft: review and prospect

更新时间：2026-05-28

- Integrated scheme of air-breathing high-speed aircraft: review and prospect
- Vol. 41, Issue 8, Pages: 13-25(2023)
- 作者机构：
  
  国防科技大学空天科学学院，高超声速冲压发动机技术重点实验室,长沙,410073
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0116
  CLC： V221
- Published：2023
- 稿件说明：
移动端阅览
王振国, 梁剑寒, 范晓樯, 等. 吸气式高速飞行器一体化方案：回顾与展望[J]. 空气动力学学报, 2023, 41(8): 13−25.

WANG Zhenguo, LIANG Jianhan, FAN Xiaoqiang, et al. Integrated scheme of air-breathing high-speed aircraft: review and prospect[J]. 2023, 41(8): 13-25.
王振国, 梁剑寒, 范晓樯, 等. 吸气式高速飞行器一体化方案：回顾与展望[J]. 空气动力学学报, 2023, 41(8): 13−25. DOI： 10.7638/kqdlxxb-2023.0116

WANG Zhenguo, LIANG Jianhan, FAN Xiaoqiang, et al. Integrated scheme of air-breathing high-speed aircraft: review and prospect[J]. 2023, 41(8): 13-25. DOI： 10.7638/kqdlxxb-2023.0116.

摘要

通过梳理吸气式高速飞行器一体化发展脉络，回顾和分析了技术验证、实用化和未来重复使用阶段飞行器一体化方案的主要研究内容和关键进展。在技术验证阶段，设计者针对轴对称构型和升力体构型提出多种一体化方案及对应设计方法，有力支撑了高速飞行技术验证，丰富了一体化设计理论。在实用化阶段，高速飞行技术工程应用对一体化提出严苛的约束，一体化主要解决流量捕获、设备装载和升阻比之间的矛盾，逐渐形成腹部进气布局一体化方案。针对未来重复使用飞行器，更多样的动力模式、更复杂的气动外形对一体化设计提出更高要求，高效、宽范围的动力系统、高度一体化的翼身融合构型、更优的进气布局方案是吸气式高速飞行器一体化设计的重要发展方向。

Abstract

This article reviews and analyzes the main research contents and key progress of the integrated development of air-breathing high-speed aircraft

including the stages of technology validation

practical application

and future reusable aircraft integration schemes. In the technology validation stage

designers proposed various integrated schemes and corresponding design methods for axisymmetric configurations and lifting-body configurations

which provided strong support for high-speed flight technology validation and enriched the design theory of integrated schemes. In the practical application stage

the engineering application of high-speed flight technology imposes stringent constraints on integration. The integration mainly addresses the conflicts between flow capture

equipment payload

and lift-to-drag ratio

gradually forming integrated schemes with belly intake layouts. For future reusable aircraft

a greater variety of propulsion modes and more complex aerodynamic shapes impose higher requirements on integration design. Efficient and wide-range power systems

highly integrated wing-body blended configurations

and more advanced intake layout schemes are important directions for the integrated design of air-breathing high-speed aircraft.

关键词

Keywords

references

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