If the flame is propagating at steady speed in static and homogeneous clouds, flow field just behind the pressure waves is self-similar.
若火焰以稳定速度在均匀的静止云雾中传播，则压力波后的流场是自相似的。
In order to make the experiments environment close to the real network, in the experiments of verifying fairness of algorithm we use self-similar flow as the background flows.
为了使实验环境更接近现实网络，在验证算法的公平性的试验中使用了自相似的背景流来模拟网络的状态变化。
On the basis of a self-similar solution as well as of the assumption, of the "Transverse Motion", a general linear theory on hypersonic flow over a general slender body is set up in this paper.
本文在平面截面的假定下，以幂次自模拟解为基础，提出了高超音速气流绕一般细长（辶回）转体流动的普遍线性化理论。
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