Method of curved-shock characteristics with application to inverse design of supersonic flowfields
C Shi, C Zhu, Y You, G Zhu - Journal of Fluid Mechanics, 2021 - cambridge.org
This paper describes the development of a method of curved-shock characteristics based on
curved shock theory. The proposed method is applied to supersonic flowfield calculations …
curved shock theory. The proposed method is applied to supersonic flowfield calculations …
[HTML][HTML] 高超声速进气道飞行器一体化设计技术的发展
孟宇鹏， 杨晖， 满延进 - 气体物理, 2021 - xml-data.org
对高超声速进气道与飞行器一体化设计技术和发展进行了研究, 包含轴对称压缩, 二维压缩,
侧压以及内压缩进气道在高超声速飞行器上的典型布局设计方案. 对高超声速可调进气道类型 …
侧压以及内压缩进气道在高超声速飞行器上的典型布局设计方案. 对高超声速可调进气道类型 …
[图书][B] Design of Streamline-Traced Inlets and Their Integration with Rotating Detonation Engines
ML Branch - 2021 - search.proquest.com
This thesis has two parts: 1) design of the streamline-traced inlets (STIs); and 2) integration
of STIs with rotating detonation engines (RDEs). The STI design starts with a two …
of STIs with rotating detonation engines (RDEs). The STI design starts with a two …