1) terminal shock
结尾正激波
1.
A series of numerical computation have been conducted to characterize the movement of the terminal shock inside an axisymmetric supersonic inlet under perturbation pressure with different amplitudes and frequencies.
采用有限体积法计算了某轴对称超声速进气道,在不同幅度和频率的出口扰动压强下的进气道内结尾正激波的运动情况,得出了进气道内结尾正激波运动特性和扰动压强的频率和幅度的关系。
2) tail shock wave; trailing (edge) shock wave
尾激波
3) tail shock wave
尾部激波
4) trailing shock wave
尾冲波，尾激波
5) laser wakefields
激光尾波场
1.
More importantly, they can drive large-amplitude plasma waves, so called the laser wakefields, which can accelerate electrons to the energy of hundreds of MeV in mm-length.
而更重要的是超短激光脉冲可以通过其有质动力激发大振幅的等离子体波(称为激光尾波场),后者可以在毫米空间尺度把电子加速到上百兆电子伏的能量。
6) normal shock wave
正激波
1.
The optimum characteristics of the gas dynamic parameters for the shock wave system , which is made of the regular reflection shock wave with a normal shock wave in the supersonic flow is studied.
研究了超音速气流中正规反射激波加一正激波结构下的参数优化特性 ,给出了求解这种优化结构的方法。
补充资料：结尾
结束的阶段：～工程 ㄧ文章的～写得很精彩。
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参考词条