A wake flow with relatively lower pressure and recirculation zone exists on the lee side of the injector.
在喷口后的背风区，存在具有低压和回流区的尾迹。
In this paper, plasma wake flow of hypersonic reentry vehicle and radar scattering characteristics have been studied.
对再入飞行器等离子体尾迹及其雷达散射特性进行了分析、研究和大量的计算。
The result shows that there exists neither flow separation nor apparent wake flow within an non-overload centrifugal impeller.
结果表明，无过载离心叶轮内部流动既没有出现分离，也没有明显的尾迹区存在。
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