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contributor authorLuo, Mingcong
contributor authorZheng, Qun
contributor authorSun, Lanxin
contributor authorDeng, Qingfeng
contributor authorYang, Junjie
date accessioned2017-05-09T01:13:31Z
date available2017-05-09T01:13:31Z
date issued2014
identifier issn0889-504X
identifier otherturbo_136_03_031016.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156577
description abstractIn this paper, wet compression effect on an eightstage axial subsonic compressor is simulated by steady numerical methods. Special attention is paid to the compressor design operating condition and rotating stall boundary to contrast and analyze the changes, such as the compressor performance and the flowfield characteristics under dry and wet conditions. The motions of water droplets are also simulated and analyzed. The results indicate that wet compression could weaken or eliminate the flow separation; improve the flow capacity, efficiency, and pressure ratio of this compressor; and make the compressor operating near the rotating stall boundary enter into the normal working condition.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of Wet Compression on a Multistage Subsonic Compressor
typeJournal Paper
journal volume136
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4025198
journal fristpage31016
journal lastpage31016
identifier eissn1528-8900
treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 003
contenttypeFulltext


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