Article ID Journal Published Year Pages File Type
8058392 Aerospace Science and Technology 2017 12 Pages PDF
Abstract
Numerical simulations were performed to analyze the flow characteristic, variation of total temperature and development of swirl flow in the stator well. Besides, CFD results could provide more detailed insight into the flow mechanisms that are responsible for the influences of rotation and tip clearance.
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Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
Preview
Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well
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