tip-leakage flow

基本解釋

Upstream stator-rotor interaction reduces the double leakage flow intensity in the rotor tip region.
上游靜葉干涉減少了動葉頂部二次泄漏流強度。
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Three-dimensional flow of the tip leakage vortex inside an axial-flow compressor rotor passage was studied using a 3-D Laser Doppler Velocimetry.
用三維激光多普勒測速系統(tǒng)測量了軸流壓氣機設計狀態(tài)轉(zhuǎn)子葉尖泄漏渦+和尾跡在靜子尖區(qū)的傳播過程。
In this paper, the influence of tip leakage flow on the 3-D viscous flow field is investigated for different blade tip gap shapes under the condition of rotating hub or stationary hub.
本文針對幾種不同形態(tài)的葉柵頂部間隙，在環(huán)壁轉(zhuǎn)動與靜止的不同情況下，研究間隙內(nèi)的泄漏流動對三維粘性流場的影響。
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