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5. Research on the Effect of the Radius of Forebody Leading Edge on the Characteristic of SWBLI on Hype

Research on the Effect of the Radius of Forebody Leading Edge on the Characteristic of SWBLI on Hype

来源 :第六届亚洲推进与动力国际会议 | 被引量 : 0次 | 上传用户：hyxh4388488

【摘 要】

：

Shock wave/boundary layer interaction (SWBLI) on hypersonic inlet external compression surface has remarkably influence on the inlet performance,and the characteristic of SWBLI on the forebody of airc

【作 者】

：

WANG Zhenfeng XIE Aimin JIANG Tao 

【机 构】

：

Science and Technology on Scramjet Laboratory,Hypervelocity Aerodynamics Institute of CARDC,Mianyang

【出 处】

：

第六届亚洲推进与动力国际会议

【发表日期】

：

2012年9期

【关键词】

：

Hypersonic inlet External compression surface Focusing schlieren Shock Wave/Boun 

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论文部分内容阅读

　　Shock wave/boundary layer interaction (SWBLI) on hypersonic inlet external compression surface has remarkably influence on the inlet performance,and the characteristic of SWBLI on the forebody of aircraft is influenced by the radius of forebody leading edge.

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