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带根部间隙压气机静叶流道流动结构研究
引用本文:陆华伟,郭爽,钟兢军,张凯,陈浮,丁小娟.带根部间隙压气机静叶流道流动结构研究[J].工程热物理学报,2012(1):51-54.
作者姓名:陆华伟  郭爽  钟兢军  张凯  陈浮  丁小娟
作者单位:大连海事大学轮机工程学院;哈尔滨工业大学能源科学与工程学院;中国舰船研究设计中心
基金项目:国家自然科学基金资助项目(No.50646021);“中央高校基本科研业务费专项资金”资助项目
摘    要:本文采用数值模拟的方法对某低速压气机静叶流道内的流动结构进行了研究。设计工况下,带根部间隙的静叶流道中主要存在三个大尺度旋涡结构,分别为上通道涡、刮削涡和集中脱落涡,这些涡系在生成和发展过程中相互作用,流道内总奇点数先增加后减小,但都严格遵循了流道奇点数拓扑法则。

关 键 词:压气机  静叶流道  旋涡结构  奇点

Investigation of Flow Structure in Compressor Stator Passage With Hub Tip
LU Hua-Wei,GUO Shuang,ZHONG Jing-Jun,ZHANG Kai,CHEN Fu,DING Xiao-Juan.Investigation of Flow Structure in Compressor Stator Passage With Hub Tip[J].Journal of Engineering Thermophysics,2012(1):51-54.
Authors:LU Hua-Wei  GUO Shuang  ZHONG Jing-Jun  ZHANG Kai  CHEN Fu  DING Xiao-Juan
Institution:1 (1.Marine Engineering College,Dalian Maritime University,Dalian 116026,China; 2.School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China; 3.China Ship Development and Design Center,Wuhan 430064,China)
Abstract:Numerical investigation of flow structure was done in a low speed axial compressor’s stator passage.There are three large vortexes exist in the stator passage with blade hub tip at design condition.They are the passage vortex at up side,the scraping vortex near hub tip and the concentrated shed vortex.These vortexes interact each other at their generation and development proceeding.The total number of singular points increases at first and decreases at last.But it obeys the rule of singular points number in the passage.
Keywords:compressor  stator passage  vortex structure  wake interference
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