首页 | 本学科首页   官方微博 | 高级检索  
     检索      

大小叶片轴流压气机转子流动特性分析
引用本文:严明,陈懋章.大小叶片轴流压气机转子流动特性分析[J].推进技术,2002,23(4):280-282.
作者姓名:严明  陈懋章
作者单位:北京航空航天大学,动力系,北京,100083
摘    要:采用全三维粘性数值模拟手段,通过与按常规设计转子对比的方法,分析研究了大小叶片轴流压气机转子流动特性,分析结果表明,大小叶片转子流场在叶根亚声速区的流通能力增强,在叶尖跨声速区可以产生更加有利的激波体系,小叶片可以有效地控制叶栅槽道中气流扩散,在较高负荷和相同喘振裕度的条件下,大小叶片转子可以比按常规设计的转子在更高的压比,效率和流量下工作。

关 键 词:叶片  轴流压气机  转子  流动特性  数值计算  纳维尔-斯托克斯方程
文章编号:1001-4055(2002)04-0280-03
修稿时间:2001年8月22日

Flow performance analysis in an axial compressor rotor with splitter
YAN Ming and CHEN Mao,zhang.Flow performance analysis in an axial compressor rotor with splitter[J].Journal of Propulsion Technology,2002,23(4):280-282.
Authors:YAN Ming and CHEN Mao  zhang
Institution:Dept of Jet Propulsion, Beijing Univ of Aeronautics and Astronautics,Beijing 100083,China;Dept of Jet Propulsion, Beijing Univ of Aeronautics and Astronautics,Beijing 100083,China
Abstract:The flow characteristics of one axial compressor rotor with splitter and two normally designed rotors with different solidities were analyzed by the 3 D viscous code The comparison shows that the mass flux in hub region was large and the shock wave system in tip region was desired The analysis results show that the flow diffusion was effectively controlled by splitter According to the calculated characteristics,the rotor with splitter can be operated with higher total pressure ratio, higher efficiency and larger mass flow than normally designed rotors, under the high loaded condition and with the same surge margin
Keywords:Compressor blade  Axial flow compressor  Rotor  Numerical calculation  Navier  Stokes equation
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号