The instability and loss of flow increase because of the complex profile of inlet box and unreasonable axile bush structure,which also induce circumferential asymmetry of downstream flow.
英
美
释义
进气箱的复杂形状和不合理的轴套结构会增大流动的不稳定性和损失,并引起了下游流动的周向不均匀性。
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