It can be concluded that the accelerator mode MHD-controlled inlet can improve the inlet performance when the flight Machnumber is lower than the design value.
研究结果表明，当飞行马赫数小于设计马赫数时加速器模式的磁控进气道可以提高进气道的性能。
2
The Machnumber at cascade inlet increasing range was larger with the slot width increased.
缝隙宽度的增大使叶栅进口马赫数升高的幅度也越大。
3
In ejector and ramjet modes, working over a wide Machnumber range is very important for the RBCC inlet, so the 2d RBCC inlet should be variable-geometry.