The turbulent flow in 2 D mixed compression supersonicinlet is simulated by numerical method.
对二元混压超音速进气道湍流流场进行了数值模拟。
2
The performance of supersonicinlet determines the pressure and the air flux in combustor, then affect the work of ramjet.
超声速进气道的性能优劣决定了补燃室流场内的压强和空气流量，进而影响到冲压发动机的工作性能。
3
The numerical simulation of supersonicinlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit TVD.