tip-leakage flow

基本解释

Upstream stator-rotor interaction reduces the double leakage flow intensity in the rotor tip region.
上遊靜葉乾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測量了軸流壓氣機設計狀態轉子葉尖泄漏渦+和尾跡在靜子尖區的傳播過程。
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的葉柵頂部間隙，在環壁轉動與靜止的不同情況下，研究間隙內的泄漏流動對三維粘性流場的影響。
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