| 摘要: |
| 乘波体是一种典型的高速气动构型，由于高升阻比和均匀的下表面流动等特性使其成为机身/进气道一体化设计的理想构型。随着对乘波体设计方法的不断研究，提高乘波体在非设计条件下的气动性能，实现乘波体的宽速域飞行成为乘波体实用化的一个重要研究方向。将目前的宽速域乘波体设计方法分成变马赫数、多级组合和涡波结合3种类型，并详细介绍了这些方法的设计过程，分析了设计方法的优缺点。 |
| 关键词: 乘波体 宽速域 设计方法 气动外形 |
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| Review on the Design Methodology of Waverider for a Wide-Speed Range |
| LUO Shibin,ZHOU Jiaming |
| (School of Aeronautics and Astronautics, Central South University) |
| Abstract: |
| The waverider is a typical high velocity aerodynamic configuration. Due to its high lift-drag ratio and uniform lower surface flow characteristics, it has become an ideal configuration for the integrated fuselage / intake design. With the continuous research on the design method of the waverider, improving the aerodynamic performance of the waverider under non-design conditions, and realizing the wide-speed flight of the waverider have become an important research direction of the waverider practicality. This paper divides the current design methods of wide-speed waverider into three types: variable Mach number, multi-stage combination and combination of shock and vortex. The design process of these methods is introduced in detail, and the advantages and disadvantages of these design methods are analyzed. |
| Key words: Waverider Wide-speed range Design method Aerodynamic configuration |