The categorization is based on 4 parameters, namely, flight height, flightMachnumber, engine rotational speed and overload on the engine center of gravity.
选取了飞行高度、飞行马赫数、发动机转速以及发动机重心法向过载等4个参数作为分类的原始依据参数。
2
It can be concluded that the accelerator mode MHD-controlled inlet can improve the inlet performance when the flightMachnumber 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。
3
It is necessary to simulate the high enthalpy, high pressure, Machnumber and the same concentration of oxygen species as air in hypersonic flight.