The Study of the Tip Clearance Flow of Compressor Blades
碩士 === 國立成功大學 === 航空太空工程學系 === 85 === A CFD technique is employed in the study about the tip clearance flow of compressor blades. The influence of the tip clearance on the compressor performance is mainly from the two vortices and theirint...
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| Format: | Others |
| Language: | zh-TW |
| Online Access: | http://ndltd.ncl.edu.tw/handle/10158227696534000383 |
| Summary: | 碩士 === 國立成功大學 === 航空太空工程學系 === 85 === A CFD technique is employed in the study about the tip clearance
flow of compressor blades. The influence of the tip clearance on
the compressor performance is mainly from the two vortices and
theirinteractions. One is the passage vortex and the other is
the leakage vortex.An optimum tip clearance is observed.
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