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

30°预旋进气旋转盘流动与换热特性的实验
引用本文:罗翔,徐国强,陶智,丁水汀.30°预旋进气旋转盘流动与换热特性的实验[J].北京航空航天大学学报,2007,33(3):290-293.
作者姓名:罗翔  徐国强  陶智  丁水汀
作者单位:北京航空航天大学 航空发动机气动热力重点实验室, 北京 100083
摘    要:用实验的方法对具有30°预旋进气的旋转盘附近冷气流动与换热特性进行了研究,得到了静 盘表面压力、转盘表面温度、局部努赛尔特数的分布及平均努赛尔特数的变化.结果显示静 止盘罩表面的压力随着半径的增加而增加,随转速的增加而增加.转盘表面的局部努赛尔特 数在r<0.7R的区域基本不变, r>0.7R的区域里, 局部努赛尔特数随r的增加而增大.该预旋 角情况下,进气雷诺数对盘面平均努赛尔特数的影响大于旋转雷诺数.

关 键 词:燃气轮机  涡轮转子  涡轮静子  压力分布  换热系数
文章编号:1001-5965(2007)03-0290-04
收稿时间:2006-04-26
修稿时间:2006-04-26

Flow and heat transfer in rotor-stator system with pre-swirl angle of 30°
Luo Xiang,Xu Guoqiang,Tao Zhi,Ding Shuiting.Flow and heat transfer in rotor-stator system with pre-swirl angle of 30°[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(3):290-293.
Authors:Luo Xiang  Xu Guoqiang  Tao Zhi  Ding Shuiting
Institution:National Key Laboratory on Aero-Engines, Beijing University of Aeronau tics and Astronautics, Beijing 100083, China
Abstract:An experimental study of the flow and heat transfer characteristics in a pre-sw irl rotor-stator system was described. Pre-swirl cooling air thr ough nozzles with angle of 30° in the stator flows radially outwards and leav es system from the clearance between rotor and stator. The distributions of the pressure on the stator surface, temperature, local and averaged Nusselt number o n the rotating disk surface were obtained from the tests. The experiments reveal that the pressure on the stator surface increase as the radius and also increas e as rotating speed. The local Nu number will keep invariable when r<0.7R(R is effective radius of rotating disk) in the rotating disk surface, but it will inc rease rapidly as radius when r>0.7R. The cooling flow rate have more effects on average Nu number than rotating speed in this pre-swirl angle.
Keywords:gas turbines  rotors  stators  pressure distribution  heat transfer coefficients
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》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