In this paper, the shear layer oscillation mechanism is analyzed producing and impacting which aiming at the flow circs of the jet flow simulation.
本文针对伺服阀前置级射流流场的流动情况，分析了产生和影响剪切层振荡的机理。
The oscillation of the shear layer decreases with the increase of the plate length.
随着腔内平板长度的增加，剪切层振荡的程度有所减小。
The oscillation of the shear layer decreases with the increase of the plate length.
随着腔内平板长度的增加，剪切层振荡的程度有所减小。
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