hypersonicinlet相关论文
Research on the Effect of the Radius of Forebody Leading Edge on the Characteristic of SWBLI on Hype
Shock wave/boundary layer interaction (SWBLI) on hypersonic inlet external compression surface has remarkably influence ......
The Research on Compression Corners Flow Separation State Visualization in Pulse Combustion Wind Tun
There are all kinds of compression corners in the flow path of the hypersonic crafts....
