The steady process of solid rocket motor modulated by the vortex valve is investigated theoretically.
对涡流阀调节固体火箭发动机压强的稳态过程进行了理论研究。
In this paper, we discussed the steady process in time domain and the alternative process in frequency domain.
本文对时域稳定过程和频域迭代过程进行了讨论。
The former is for steady process and the latter is especially for dynamic process that may have big fluctuation.
而对波动较大,采样点较多的动态过程必须用插值法才能真实反映这种波动。
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